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Journal articles on the topic 'Metal-reinforced laminate'

Author: Grafiati

Published: 5 June 2025

Last updated: 16 July 2025

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1

Stoll, Matthias, Franziska Stemmer, Sergej Ilinzeer, and Kay André Weidenmann. "Optimization of Corrosive Properties of Carbon Fiber Reinforced Aluminum Laminates due to Integration of an Elastomer Interlayer." Key Engineering Materials 742 (July 2017): 287–93. http://dx.doi.org/10.4028/www.scientific.net/kem.742.287.

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Fiber-Metal-Laminates (FML) show superior dynamic mechanical properties combined with low densities. The mechanical performance of for example commercially available fiber-metal-laminate, glass laminate aluminum reinforced epoxy, can be improved by the substitution of glass fibers with carbon fibers. However, carbon fiber reinforced aluminum laminate introduces a mismatch of coefficients of thermal expansion and the possibility of galvanic corrosion. The fiber-metal-laminate is altered by the integration of an elastomer interlayer which is desired to solve both problems. The high electrical re

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2

Salve, Aniket, Ratnakar Kulkarni, and Ashok Mache. "A Review: Fiber Metal Laminates (FML’s) - Manufacturing, Test methods and Numerical modeling." International Journal of Engineering Technology and Sciences 3, no. 2 (2016): 71–84. http://dx.doi.org/10.15282/ijets.6.2016.1.10.1060.

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Weight reduction of components is the main aim of different industrial sectors. This leads to increasing application areas of fiber composites for primary structural components. Aiming this objective, a new lightweight Fiber/Metal Laminate (FML) has been developed. Fiber metal laminate is one such material which is being widely investigated for its performance compared to existing material.. The most commercially available fiber metal laminates (FML’s) are ARALL (Aramid Reinforced Aluminium Laminate), based on aramid fibers, GLARE (Glass Reinforced Aluminium Laminate), based on high strength g

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3

Lu, Hongbin, Dongfa Sheng, Yuting Fang, Hongquan Yu, and Fan Yang. "Analysis of Tensile Failure Behavior of Metal Fiber Laminates Under Different Temperature Environments." Polymers 16, no. 23 (2024): 3319. http://dx.doi.org/10.3390/polym16233319.

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The tensile properties of fiber metal laminates were examined at temperatures ranging from 30 °C to 180 °C in this paper through the integration of numerical simulation techniques, experimental measurements, and digital image correlation techniques. The laminates were initially modeled using finite elements, and the failure behavior of porous basalt-fiber-reinforced aluminum alloy plates was numerically simulated. Consequently, metal fiber laminate stress–strain responses were varied by numerous tensile experiments conducted at varying temperatures. Simultaneously, a scanning electron microsco

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4

Frankiewicz, Mariusz, Grzegorz Ziółkowski, Robert Dziedzic, Tomasz Osiecki, and Peter Scholz. "Damage to inverse hybrid laminate structures: an analysis of shear strength test." Materials Science-Poland 40, no. 1 (2022): 130–44. http://dx.doi.org/10.2478/msp-2022-0016.

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Abstract Hybrid laminates with continuous fiber reinforcement, such as glass reinforced aluminium laminate (GLARE), aramid reinforced aluminum laminate (ARALL), or carbon reinforced aluminum laminate (CARALL), have been developed to increase the lightweight potential and fatigue resistance applied for aircraft structures. However, the use of thermosetting matrices imposes material limitations regarding recycling, malleability, and manufacturing-cycle times. The inverse hybrid laminate approach is based on a continuous fiber-reinforced thermoplastic matrix, in which a metal insert is integrated

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Vilas Boas, Cristiane, Felipe Moreno, and Demetrio Jackson dos Santos. "Mechanical Analysis of Polybenzoxazine Matrix in Fiber Metal Laminates." Materials Science Forum 869 (August 2016): 215–20. http://dx.doi.org/10.4028/www.scientific.net/msf.869.215.

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In this work we investigated the application of a novel high performance polymer, polybenzoxazine, as a polymeric matrix in Fiber Metal Laminates (FML). This polymer, when applied on the development of FMLs, generated higher mechanical properties in comparison to fiber metal laminates obtained with epoxy. To investigate the mechanical performance of the polybenzoxazine matrix in FMLs, a mechanical behavior comparison was carried out among epoxy matrix laminates - glass fiber reinforced aluminum laminate (GLARE) and carbon fiber reinforced aluminum laminate (CARALL) - and FML constructed with a

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Neugebauer, Reimund, Verena Kräusel, and Alexander Graf. "Process Chains for Fibre Metal Laminates." Advanced Materials Research 1018 (September 2014): 285–92. http://dx.doi.org/10.4028/www.scientific.net/amr.1018.285.

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The combination of fibre-reinforced materials with metals is defined as a fibre metal laminate. These material composites have already been a subject of research for several years. The long manufacturing time resulting from the period required for consolidation of the thermosetting resin is a major disadvantage of the fibre metal laminates previously in use (for instance GLARE, which is a combination of aluminium with glass fibre-reinforced plastic). In this paper, a new fibre metal laminate with a thermoplastic resin in the carbon fibre-reinforced plastics (CFRP) is introduced. The applicatio

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7

Xie, Botao, Liang Gao, Shuai Jiang, Shangda Zhang, Chen Wu, and Xu Ran. "Notched tensile response and damage mechanism of the GLARE laminate." Journal of Composite Materials 54, no. 22 (2020): 3037–46. http://dx.doi.org/10.1177/0021998320907963.

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Glass laminate aluminum reinforced epoxy, as an attractive material for advanced aerospace applications, is most likely to face the challenge of various blunt notched damages. In this paper, the tensile tests of the glass laminate aluminum reinforced epoxy with circular and square blunt notches are conducted. The effects of notch geometry, such as notch diameter, notch corner radius, and off-axis angle, on the laminated tensile behaviors of glass laminate aluminum reinforced epoxy laminate are explored. A characteristic distance function representing the damage-affected region of notch is empi

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8

Feng, Ng Lin, Sivakumar DharMalingam, Kamarul Ariffin Zakaria, and Mohd Zulkefli Selamat. "Investigation on the fatigue life characteristic of kenaf/glass woven-ply reinforced metal sandwich materials." Journal of Sandwich Structures & Materials 21, no. 7 (2017): 2440–55. http://dx.doi.org/10.1177/1099636217729910.

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Fatigue life characteristic of hybrid composite reinforced metal laminate is a notable investigation since this kind of material offers several superior characteristics over conventional metallic alloy. A majority of the researches have focused on the mechanical properties of hybrid composite and conventional fibre metal laminate such as glass reinforced aluminium epoxy and aramid fibre reinforced aluminium laminate. However, investigation on the fatigue life behaviour of hybrid composite reinforced metal laminate still remains unexplored. In this study, the fatigue life characteristic of hybr

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9

Yeoh, T. S., S. Saadon, and N. Mazlan. "Fire properties test on fibre metal laminate based on carbon/flax fibre composites reinforced with silicon carbide for aircraft engine fire-designated zones." IOP Conference Series: Earth and Environmental Science 1500, no. 1 (2025): 012043. https://doi.org/10.1088/1755-1315/1500/1/012043.

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Abstract Due to the problems of flammability, weight and health risk associated with the materials in the fire designated zone of an aircraft engine, there is a need to develop new composites that will resolve the fire issues. Accordingly, new composites, the fibre metal laminates reinforced silicon carbide will be examined in this research. The fibre metal laminate composites using carbon/flax fibre will be tested with aluminium alloy. The study presents a novelty in hybridising the synthetic/natural fibre with nanocomposites in the fire designated zone of an aircraft engine. To ensure the va

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Trautmann, Maik, Selim Mrzljak, Frank Walther, and Guntram Wagner. "Mechanical Properties of Thermoplastic-Based Hybrid Laminates with Regard to Layer Structure and Metal Volume Content." Metals 10, no. 11 (2020): 1430. http://dx.doi.org/10.3390/met10111430.

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Multi layered lightweight material compounds such as hybrid laminates are composed of different layers of materials like metals and unidirectional fibre-reinforced plastics and offer high specific strength. They can be individually tailored for applications like outer cover panels for aircraft and vehicles. Many characteristics especially layer structure, volume contents of the embedded materials as well as layer surface adhesion determine the performance of a hybrid laminate. In this study, the influence of layer structure and metal volume content are evaluated with regard to the mechanical p

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11

Saadatfard, Alireza, Mahdi Gerdooei, and Abdolhossein Jalali Aghchai. "Drawing potential of fiber metal laminates in hydromechanical forming: A numerical and experimental study." Journal of Sandwich Structures & Materials 22, no. 5 (2018): 1386–403. http://dx.doi.org/10.1177/1099636218785208.

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It is known that fiber metal laminates as one of hybrid materials with thin metal sheets and fiber/resin layers have limited formability in conventional forming methods. This paper presents an experimental and numerical study for drawability of glass fiber-reinforced aluminum laminates under hydromechanical drawing technique. Fiber metal laminates comprised of a layer of woven glass fiber-reinforced prepreg, sandwiched between two layers of aluminum alloy. In order to produce fiber metal laminates, the laminates were subjected to a sufficient squeezing pressure under a controlled heating time

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12

Boczar, Kamil, Karol Wasłowicz, Andrzej Kubit, Dorota Chodorowska, and Romuald Fejkiel. "Effect of Heating and Cooling of Aluminium-Based Fibre-Metal Laminates on Their Tensile Strength." Advances in Mechanical and Materials Engineering 40 (2023): 149–57. http://dx.doi.org/10.7862/rm.2023.15.

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The widespread use of composite materials in the construction of machines encourages to better understand their properties and the impact of various external factors on these properties. Fibre metal laminates (FMLs) consist of alternating layers of metal and a polymer matrix laminate reinforced with continuous fibres. The aim of this work was to investigate the effect of cyclical temperature changes and thermal shocks (heating the sample to a high temperature in a short time) on the strength properties of FMLs from AW-1050A aluminium sheet, glass fibre fabric and carbon fibre fabric. The resea

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13

Podolak, Piotr, Magda Droździel-Jurkiewicz, Patryk Jakubczak, and Jarosław Bieniaś. "The Correlation of LVI Parameters and CAI Behaviour in Aluminium-Based FML." Materials 16, no. 8 (2023): 3224. http://dx.doi.org/10.3390/ma16083224.

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An experimental analysis of mechanical behaviour for aluminium-based fibre metal laminates under compression after impact was conducted. Damage initiation and propagation were evaluated for critical state and force thresholds. Parametrization of laminates was done to compare their damage tolerance. Relatively low-energy impact had a marginal effect on fibre metal laminates compressive strength. Aluminium–glass laminate was more damage-resistant than one reinforced with carbon fibres (6% vs. 17% of compressive strength loss); however, aluminium–carbon laminate presented greater energy dissipati

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Song, Chun Han, Khaled Giasin, Abu Saifullah, and Antigoni Barouni. "Investigation of the Contact Interface between Natural Fibre Metal Laminates under Tension Using Finite Element Analysis (FEA)." Polymers 14, no. 21 (2022): 4650. http://dx.doi.org/10.3390/polym14214650.

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Fibre Metal Laminates (FMLs) consist of layers of metals combined with layers of fibre-reinforced composites bonded together to create a laminate. The behaviour of a Fibre Metal Laminate (FML) with natural fibre composites has been investigated in this study with a specific focus on the performance of the laminate under uniaxial tension. The integration of aluminium layers with natural fibre flax/pp layers at different fibre orientations has been numerically modelled and analysed, by investigating the contact interface between natural fibre metal laminates (NFML) using finite elements (FE) imp

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15

Najafi, M., A. Darvizeh, and R. Ansari. "Effect of salt water conditioning on novel fiber metal laminates for marine applications." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 233, no. 8 (2018): 1542–54. http://dx.doi.org/10.1177/1464420718767946.

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One of the issues with the widespread use of polymer matrix composites in marine applications is their high susceptibility to environmental degradation, particularly hygrothermal conditions. Therefore, the present research intends to contribute to the better protection of the marine polymer matrix composites through the introduction of a newly developed fiber metal laminate for marine applications. This type of fiber metal laminate consists of a marine aluminum alloy of 5083 alternating with glass fiber reinforced epoxy composite layers. In order to evaluate the characterization of the environ

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16

Hindersmann, Arne, Constantin Bäns, and Lutz Beyland. "Infusion of Thick-Walled Fiber Metal Laminates with Aligned Holes in the Metal Foils." Journal of Composites Science 8, no. 7 (2024): 278. http://dx.doi.org/10.3390/jcs8070278.

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The rotor blades of wind turbines are becoming increasingly longer, which increases the diameter at the blade connection. Transport problems are the result, as the rotor blades no longer fit under highway bridges, for example. The increase in diameter can be prevented by increasing the bearing strength of the laminate using fiber metal laminates (FMLs). Individual layers of fiber material are replaced by metal foils in FMLs. This work is focused on the infusion of thick-walled FMLs, with infiltration experiments being carried out in-plane and out-of-plane. For the out-of-plane infusion tests,

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17

Zhang, Quanda, Fuzhen Sun, Rigele Ji, Zizhi Liu, Huiyu Li, and Yao Wang. "Experimental Research on the Thermal-Consolidation Compound Forming of Thermosetting Fiber Metal Laminates Design for Complex Structures with Variable Curvature." Metals 12, no. 6 (2022): 935. http://dx.doi.org/10.3390/met12060935.

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The glass fiber-reinforced metal laminates (GLARE) cannot be used to form complex laminate structures in the aerospace industry, because there is substantial variation in the plasticity of the heterogeneous materials. Hence, a compound process for composite materials based on the thermoforming technology for aluminum alloy and fiber-reinforced metal laminates (FMLs)-forming technology was proposed; it contains solution heat treatment, thermoforming, quick cold die quenching, artificial aging integrated process (HFQ), and the thermal consolidation of fiber-reinforced metal laminates, and it is

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18

Lang, Zijian, Meng Zhang, Xiaoxing Li, and Xing Huang. "Innovative Manufacturing and Application of Fiber Metal Laminate Pipe." MATEC Web of Conferences 319 (2020): 04004. http://dx.doi.org/10.1051/matecconf/202031904004.

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Fiber-reinforced metal laminate tube (FMLT) is a multi-layered ultra-hybrid material that cures at fixed pressure and temperature after alternating metal laminates and fiber composites. As with the production process similar to the second-generation GLARE fiber-reinforced metal layer, the management layer of the formed composite layer should have good impact resistance characteristics, and can also be used in the impact-resistant structure of the aircraft, the landing cushion structure of the aircraft, and the body collision Device to protect aviation materials.The composite pipe fittings are

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19

Chen, Yizhe, Zhuoqun Wang, Yi Lin, Hui Wang, and Lin Hua. "Theoretical Modeling and Experimental Verification of the Bending Deformation of Fiber Metal Laminates." Materials 16, no. 9 (2023): 3486. http://dx.doi.org/10.3390/ma16093486.

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Fiber metal laminates have been widely used as the primary materials in aircraft panels, and have excellent specific strength. Bending deformation is the most common loading mode of such components. An accurate theoretical predictive model for the bending process for the carbon reinforced aluminum laminates is of great significance for predicting the actual stress response. In this paper, based on the metal-plastic bending theory and the modified classical fiber laminate theory, a modified bending theory model of carbon-fiber-reinforced aluminum laminates was established. The plastic deformati

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20

Ding, Guoping, Wenhao Song, Xiaoling Gao, and Hao Cao. "Damage Detection in Holed Carbon Fiber Composite Laminates Using Embedded Fiber Bragg Grating Sensors Based on Strain Information." Shock and Vibration 2020 (December 7, 2020): 1–11. http://dx.doi.org/10.1155/2020/8813213.

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Compared with metal materials, Carbon Fiber Reinforced Plastic (CFRP) is more excellent in performance, with high specific strength and high specific modulus. And among various CFRP structural elements, CFRP laminated plates have widespread applications. However, some indiscernible and hidden primary damage always appears on the CFRP laminated plate and will continuously evolve and expand after being loaded. This work starts with the analysis of the relationship between the changes of the strain distribution and damage expansion of CFRP laminated plates and proposes the damage recognition meth

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21

Zhang, Zheyi, Haotian Guo, Yang Lan, and Libin Zhao. "Impact Resistance Study of Fiber–Metal Hybrid Composite Laminate Structures: Experiment and Simulation." Materials 18, no. 12 (2025): 2906. https://doi.org/10.3390/ma18122906.

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Thermoplastic carbon fiber/aluminum alloy hybrid composite laminates fully integrate the advantages of fiber-reinforced composites and metallic materials, exhibiting high fatigue resistance and impact resistance, with broad applications in fields such as national defense, aerospace, automotive engineering, and marine engineering. In this paper, thermoplastic carbon fiber/aluminum alloy hybrid composite laminates were first prepared using a hot-press machine; then, high-velocity impact tests were conducted on the specimens using a first-stage light gas gun test system. Comparative experimental

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22

Sexton, Anthony, Wesley Cantwell, Matthew Doolan, and Shankar Kalyanasundaram. "Investigation of the Deformation Behaviour of a Thermoplastic Fibre Metal Laminate." Materials Science Forum 773-774 (November 2013): 503–11. http://dx.doi.org/10.4028/www.scientific.net/msf.773-774.503.

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Fibre metal laminates are sandwich materials comprised of a fibre-reinforced composite and a metal alloy. These advanced materials offer superior properties compared to the monolithic constituents; primarily, improved specific strength and stiffness compared to metals and improved impact and fatigue resistance when compared to composite materials. The use of these advanced materials is currently restricted to specialised applications where the superior properties justify the high cost of manufacturing. The formability of a fibre metal laminate based on a glass fibre reinforced polypropylene an

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23

Mohammed, Ibrahim, Abd Rahim Abu Talib, Mohamed Thariq Hameed Sultan3, and Syamimi Sadoon. "Fire behavioural and mechanical properties of carbon fibre reinforced aluminium laminate composites for aero-engine." International Journal of Engineering & Technology 7, no. 4.13 (2018): 22. http://dx.doi.org/10.14419/ijet.v7i4.13.21323.

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Two different properties of fibre-metal laminate composites (FML), including the fire behaviour and mechanical properties, were experimentally studied in this paper. The fibre-metal laminate composites studied were made of aluminium alloy 2024-T3, carbon fibre, flax, kenaf and epoxy resin/hardener arranged in different forms. The aims of the study are to assess the fire behaviour of the composites using ISO2685 standard and mechanical properties of the composite after withstanding the burn-through according to the standard. The fire test was carried out using ISO2685 standard using a propane-a

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Sessner, Vincent, Alexander Jackstadt, Wilfried V. Liebig, Luise Kärger, and Kay A. Weidenmann. "Damping Characterization of Hybrid Carbon Fiber Elastomer Metal Laminates using Experimental and Numerical Dynamic Mechanical Analysis." Journal of Composites Science 3, no. 1 (2019): 3. http://dx.doi.org/10.3390/jcs3010003.

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Lightweight structures which consist to a large extent of carbon fiber reinforced plastics (CFRP), often lack sufficient damping behavior. This also applies to hybrid laminates such as fiber metal laminates made of CFRP and aluminum. Since they are usually prone to vibrations due to their high stiffness and low mass, additional damping material is required to meet noise, vibration and harshness comfort demands in automotive or aviation industry. In the present study, hybrid carbon fiber elastomer metal laminates (HyCEML) are investigated which are intended to influence the damping behavior of

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Sessner, Vincent, Matthias Stoll, Arnaud Feuvrier, and Kay André Weidenmann. "Determination of the Damping Characteristics of Fiber-Metal-Elastomer Laminates Using Piezo-Indicated-Loss-Factor Experiments." Key Engineering Materials 742 (July 2017): 325–32. http://dx.doi.org/10.4028/www.scientific.net/kem.742.325.

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. In technical applications components are often exposed to vibrations with a broad range of frequencies. To ensure structural integrity and a convenient usage for the customer, materials with good damping characteristics are desirable. Especially stiff and lightweight structures tend to be prone to vibrations. Fibre metal laminates (FML) offer great potential for lightweight design applications due to their good fatigue behavior. By using carbon fiber reinforced plastics (CFRP) as part of the laminates very good strength and stiffness to weight ratios can be obtained. To improve the damping c

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Safari, M., M. Salamat-Talab, A. Abdollahzade, A. Akhavan-Safar, and LFM da Silva. "Experimental investigation, statistical modeling and multi-objective optimization of creep age forming of fiber metal laminates." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 234, no. 11 (2020): 1389–98. http://dx.doi.org/10.1177/1464420720943537.

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The experimental assessment of the creep age forming performance of fiber metal laminates was considered in this study. To this end, different fiber metal laminates with the stacking sequence of [Al/02/Al] were manufactured using aluminum alloy 6061 sheets as skins along with E-glass fiber-reinforced polypropylene and E-glass fiber-reinforced polyamide 6 as two different cores. Next, a comprehensive investigation was conducted on the impacts of two main parameters in the creep forming process, i.e. the effect of time and temperature on the spring-back properties of deformed fiber metal laminat

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Guillen, F., and W. J. Cantwell. "The Fracture Properties of Fibre-Metal Laminates Based on Glass Fibre Reinforced Polyamide." Advanced Composites Letters 9, no. 3 (2000): 096369350000900. http://dx.doi.org/10.1177/096369350000900305.

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The aim of this paper is to investigate the interfacial fracture properties of a novel fibre-metal laminate based on a unidirectional glass fibre reinforced polyamide 6,6 composite. Interfacial fracture tests using a modified single cantilever beam geometry have shown that good adhesion between the aluminium and glass fibre polyamide plies can be achieved using a simple stamping operation. Further testing has shown that the basic fracture properties of this system do not depend on the cooling rate employed during consolidation of the laminates.

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Palani, Sathyaseelan, Ramesh Kumar Rajamanickam, and Narayana Dilip Raja. "MECHANICAL BEHAVIOUR OF CARBON AND JUTE FIBERS REINFORCED ALUMINIUM LAMINATES FABRICATED IN DIFFERENT STACKING SEQUENCES." Suranaree Journal of Science and Technology 30, no. 1 (2023): 010193(1–6). http://dx.doi.org/10.55766/sujst-2023-01-e01879.

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In this research work, the mechanical properties of aluminium laminates having carbon fiber reinforcement and carbon-jute fibers reinforced aluminium laminates fabricated in different stacking sequences are studied. Here the fiber metal laminates are manufactured through the hand layup technique. A compression moulding machine was used to press the laminates during the production process. In this study, carbon and jute fibers along with thin aluminium sheets are used as reinforcement. Four different stacking sequences were selected. Each arrangement is symmetric and consists of ten layers of r

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Carbas, Ricardo J. C., Miguel P. Palmares, and Lucas F. M. da Silva. "Experimental and FE study of hybrid laminates aluminium carbon-fibre joints with different lay-up configurations." Manufacturing Review 7 (2020): 2. http://dx.doi.org/10.1051/mfreview/2019027.

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The use of composite materials in industry is growing due to various technological advances in composite materials accompanied by improvements in the structural adhesives used to bond them. Fibre metal laminates (FML's) are hybrid composite structures based on thin sheets of metal alloys and plies of fibre-reinforced polymeric materials. The fibre/metal composite technology combines the advantages of metallic materials and fibre-reinforced matrix systems. The aim of the present study is to use a concept similar to that used in FML to increase the peel strength of composite materials and increa

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Arpatappeh, Fardin Asghari, Mehdi Abdollahi Azghan, and Reza Eslami-Farsani. "The effect of stacking sequence of basalt and Kevlar fibers on the Charpy impact behavior of hybrid composites and fiber metal laminates." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 234, no. 16 (2020): 3270–79. http://dx.doi.org/10.1177/0954406220914325.

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In this study, the effect of the arrangement of Kevlar and basalt fibers as the reinforcements on the Charpy impact behavior of hybrid epoxy composites was investigated. Also, the effect of adding metal plates (aluminum 2024-T3 and stainless steel 316L) into the basalt/ Kevlar fibers reinforced epoxy composites to fabricate fiber metal laminates under Charpy impact loads was studied. The fabricated fiber metal laminates in this research consisted of three metal plates and two groups of composite layers placed between them and were fabricated by the hand lay-up technique. Results indicated that

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Szymczyk, Elżbieta, Krzysztof Puchała, Jerzy Jachimowicz, and Michal Salacinski. "Influence of Metal Foil on Interface Stress State in CFRP Laminate." Solid State Phenomena 250 (April 2016): 223–31. http://dx.doi.org/10.4028/www.scientific.net/ssp.250.223.

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Various materials of high specific stiffness and strength are used in aircraft structures, therefore, methods of joining them are continually improved. Adhesive joining is the most popular method used in composite structures, however, mechanical joining is often necessary due to constructional reasons. Stress concentration around the hole (notch) and point load (fastener action) transfer into the structure are the main disadvantages of mechanical joints, especially, in composite structures. The bearing failure is the only global progressive mechanism of mechanically fastened laminates and ther

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Yang, Bin, Liang He, and Yang Gao. "Simulation on impact response of FMLs: effect of fiber stacking sequence, thickness, and incident angle." Science and Engineering of Composite Materials 25, no. 3 (2018): 621–31. http://dx.doi.org/10.1515/secm-2016-0226.

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Abstract We built a three-dimensional finite element (FE) model to investigate the impact response of fiber-metal laminates (FMLs). This FE model comprises two metal layers as facesheets and a carbon woven fabric-reinforced plastic laminate as inner core. Simulation was performed on ABAQUS/Explicit platform, and stiffness progressive degeneration criteria were implemented to evaluate damages in composites. The Johnson-Cook model was selected to calculate failures in metal, while surface-based cohesive behavior was adopted to simulate the delamination phenomenon. We studied the fiber stacking s

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Kuhtz, M., N. Buschner, T. Henseler, et al. "An experimental study on the bending response of multi-layered fibre-metal-laminates." Journal of Composite Materials 53, no. 18 (2019): 2579–91. http://dx.doi.org/10.1177/0021998319835595.

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The combination of thin light metal sheets with fibre-reinforced thermoplastic layers in multi-layered fibre-metal-laminates advantageously combines the properties of both material classes. In this way, components can be developed which have both significantly increased specific properties (strength and stiffness with respect to density) and high energy absorption capacity compared with conventional design with mono materials. However, the structural behaviour of crash structures is decisively determined by material behaviour of the thermoplastic and metal constituents as well as the interface

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Zolkiewski, Sławomir. "Mechanical Properties of Fibre-Metal Composites Connected by Means of Bolt Joints." Advanced Materials Research 837 (November 2013): 296–301. http://dx.doi.org/10.4028/www.scientific.net/amr.837.296.

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The fibre-metal laminates made of a steel plate and fibreglass laminate plate were tested in the special laboratory stands. Epoxy resin and polyester resin were used as matrix to fabricate the composites. The fibre-metal laminates combine advantages of metals and laminates. These materials have very good force versus displacement characteristics and overall mechanical properties. They are very popular and widely applied in technical systems. They can be put to use in connecting materials made of various fabrics, connecting high number layer laminates and most of all connecting metals and lamin

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Sharma, Ankush P., Sanan H. Khan, and Venkitanarayanan Parameswaran. "Response and failure of fiber metal laminates subjected to high strain rate tensile loading." Journal of Composite Materials 53, no. 11 (2018): 1489–506. http://dx.doi.org/10.1177/0021998318804620.

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The tensile behavior of fiber metal laminates consisting of layers of aluminum 2024-T3 alloy and glass fiber reinforced composites under high strain rate loading is investigated. Fiber metal laminates having four different layups, but all having the same total metal layer thickness, were fabricated using a combined hand lay-up cum vacuum bagging method. The fiber metal laminate specimens were loaded in high strain rate tension using a split Hopkinson tensile bar. The rate-dependent behavior of the glass fiber composite was also obtained as baseline data. The strain on the gage area of the spec

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Iqbal, Mohd, M. S. Satrianda, Teuku Firsa, Said Amir Azan, and Laxman B. Abhang. "Bending Strength of Fiber Metal Laminate Based on Abaca Fiber Reinforced Polyester and Aluminum Alloy Metal Sheet." Key Engineering Materials 892 (July 13, 2021): 134–41. http://dx.doi.org/10.4028/www.scientific.net/kem.892.134.

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The Fiber Metal Laminate (FML) discussed here was made from Fiber Reinforced Polymer (FRP) composite, laminated by aluminum alloy sheet. The FRP composite panel was made from abaca fiber and polyester resin matrix. The objective was to study the bending strength of the FML with different fiber content. Five panels of abaca FRP were prepared using hand-lay-up methods. The weight content of the fiber in the panels were 0%, 3.56%, 5.18%, 8.94% and 12.22% respectively. The aluminum alloy sheet was laminated to the composite panel using epoxy super glue. The density of the FMLs were measured to con

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Ball, D. L., and W. S. Chan. "A Constitutive Model for Distributed Microcracking In Titanium Matrix Composite Laminae." Journal of Engineering Materials and Technology 122, no. 4 (2000): 469–73. http://dx.doi.org/10.1115/1.1289286.

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The ply constitutive relations of an energy-based model for distributed microcracking in continuous fiber reinforced metal matrix composites are presented. Simple models for damage progression are used in conjunction with these damage dependent constitutive relations to allow the prediction of fatigue life under constant amplitude, isothermal conditions. The microcracking model is discussed in the context of fatigue analysis of unnotched titanium matrix composite laminates. Analytical results generated by using this model in a unidirectional laminate analysis algorithm are presented and compar

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Fejkiel, Romuald, and Krystian Skwara. "Analysis of the thermal expansion coefficient of glass- and carbon-fibre-reinforced composites." Advances in Mechanical and Materials Engineering 41 (2024): 17–26. http://dx.doi.org/10.7862/rm.2024.2.

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With the development of manufacturing processes, an increase in the importance of metal-fibre composites in materials engineering is observed. These are materials consisting of appropriately arranged layers of metal and various types of fibres. The very wide use of composite materials in the construction of machine and equipment components means they are often exposed to work in variable temperature conditions. The aim of this article was analysis of the thermal expansion of typical composites: carbon fibre-reinforced polymer, glass fibre-reinforced polymer, glass-reinforced aluminium laminate

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Kalfountzos, Costas D., George S. E. Bikakis, and Efstathios E. Theotokoglou. "Deterministic and probabilistic buckling response of fiber–metal laminate panels under uniaxial compression." Aircraft Engineering and Aerospace Technology 94, no. 5 (2021): 745–59. http://dx.doi.org/10.1108/aeat-02-2021-0044.

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Purpose The purpose of this paper is to study the deterministic elastic buckling behavior of cylindrical fiber–metal laminate panels subjected to uniaxial compressive loading and the investigation of GLAss fiber-REinforced aluminum laminate (GLARE) panels using probabilistic finite element method (FEM) analysis. Design/methodology/approach The FEM in combination with the eigenvalue buckling analysis is used for the construction of buckling coefficient–curvature parameter diagrams of seven fiber–metal laminate grades, three glass-fiber composites and monolithic 2024-T3 aluminum. The influences

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Rauf, Obaid Ur, Aqeel A. Khurram, Rizwan Hussain, et al. "Nanoparticles enhanced interfaces of Glass fiber laminate aluminum reinforced epoxy ( GLARE ) fiber metal laminates." Polymer Composites 42, no. 8 (2021): 3954–68. http://dx.doi.org/10.1002/pc.26107.

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Osiecki, Tomasz, Colin Gerstenberger, Tristan Timmel, et al. "Inverse Hybrid Laminate for Lightweight Applications." Key Engineering Materials 847 (June 2020): 40–45. http://dx.doi.org/10.4028/www.scientific.net/kem.847.40.

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Because of their high specific stiffness and strength, fiber reinforced plastics (FRP) are preferred lightweight materials. Recent developments show a growing industrial interest in the integration of thermoplastic FRP in complex structures for high volumes. However, there are still shortcomings for these materials concerning the insufficient energy absorption in case of failure and the limited opportunities available for the assembly with other components. Improvements in the crash performance can be achieved for instance with the selective reinforcement of the FRP structure with ductile meta

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Chen, Yujie, Kai Jin, Huaguan Li, et al. "Effect of peer ply and cooling rate on the tensile properties of Al/Gf/PP laminate prepared by hot pressing." Journal of Sandwich Structures & Materials 22, no. 8 (2018): 2567–81. http://dx.doi.org/10.1177/1099636218802473.

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The glass fiber-reinforced polypropylene/AA2024 hybrid composite (short for Al/Gf/PP laminate) was prepared by hot pressing with anodized 2024-T3 aluminum alloy as the skin and thermoplastic glass fiber-reinforced polypropylene core as a substitute of thermosetting glass fiber-reinforced polymer (based on epoxy) in order to increase the productivity and reduce the production costs during manufacturing procedure. The effect of peel ply (release cloth) and cooling rate on the laminate was investigated elaborately in this work. The orientation of glass fiber is mainly influenced by the peel ply s

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Zhang, Xiaochen, Weiying Meng, Jiancheng Guo, and Yu Zhang. "Available Relevant Study on Stress Analysis and Static Strength Prediction of Fiber Metal Laminates." Scanning 2020 (November 30, 2020): 1–13. http://dx.doi.org/10.1155/2020/8874830.

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Fiber metal laminates (FMLs) are a novel type of structural material that has been extensively applied in the aerospace field. These laminates are sandwich-type composite materials that comprise alternate metal and fiber-reinforced resin layers. Because of the structural characteristics of the material, it has high-impact resistance from the metal layer and increased fracture toughness and excellent fatigue and damage tolerance properties from the fiber layer. To further develop and apply this new composite material, it is essential to understand the research status on the stress analysis of e

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Irani, Missam, Moritz Kuhtz, Mathias Zapf, et al. "Investigation of the Deformation Behaviour and Resulting Ply Thicknesses of Multilayered Fibre–Metal Laminates." Journal of Composites Science 5, no. 7 (2021): 176. http://dx.doi.org/10.3390/jcs5070176.

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Multilayered fibre–metal laminates (FMLs) are composed of metal semifinished products and fibre-reinforced plastics, and benefit from the advantages of both material classes. Light metals in combination with fibre-reinforced thermoplastics are highly suitable for mass production of lightweight structures with good mechanical properties. As the formability of light metal sheets is sometimes limited at room temperature, increasing the process temperature is an appropriate approach to improve formability. However, the melting of thermoplastic materials and resulting loss of stiffness limit the pr

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Ren, Mingfa, Fei Weng, Jing Sun, Ke Tang, Lina Feng, and Rong Chen. "Influence of Weakening Groove on Cutting Results of Composites Subjected to Shaped Charge Jet." Shock and Vibration 2021 (March 10, 2021): 1–12. http://dx.doi.org/10.1155/2021/5528574.

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Carbon-fiber-reinforced polymer (CFRP) has been widely used in aerospace structures for its high strength to weight ratio and high stiffness to weight ratio. However, current pyrotechnic separation devices are mainly made of metal materials, the cutting research on CFRP composites is limited, and the effect of weakening groove on cutting results of composites is unclear under the action of shaped charge jet. In this paper, there firstly established a three-dimensional model of explosive cutting of CFRP composites by nonlinear finite element analysis (FEA), and based on the separation time, del

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Pakseresht, M., R. Ansari, and MK Hassanzadeh-Aghdam. "Laminate analogy approach for the effective elastic properties of metal matrix nanocomposites filled with randomly dispersed graphene nanoplatelets." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 234, no. 6 (2019): 1212–19. http://dx.doi.org/10.1177/0954406219888958.

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In this study, the laminate analogy technique is utilized to calculate the elastic properties of metal matrix nanocomposites filled with graphene nanoplatelets. The graphene nanoscale fillers are the most commonly used form of graphene inclusions, which are mostly considered to be disk-shaped. With the help of the Eshelby tensor, the effects of three different shapes of graphene inclusions on the mechanical response are examined. Combining layers of metal matrix composite lamina reinforced by uniformly dispersed graphene inclusions, which are aligned differently in each layer, the metal matrix

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Zhang, Quanda, Zeen Liu, Guopeng Song, et al. "Interlayer Friction Mechanism and Scale Effects in Ultra-Thin TA1 Titanium Alloy/Carbon Fiber-Reinforced Plastic Laminates." Metals 14, no. 12 (2024): 1369. https://doi.org/10.3390/met14121369.

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Fiber metal laminates (FMLs) are a novel lightweight composite material, predominantly utilized in the aerospace sector for large-scale components like skin panels and fuselages. However, research on FMLs in the microsystem domain remains limited. Additionally, they are influenced by scale effects, rendering macroscopic forming theories inadequate for microforming applications. The application of ultra-thin fiber metal laminates in the microsystem field is hindered by this constraint. This paper investigates the friction performance of ultra-thin TA1 titanium alloy/carbon fiber-reinforced plas

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Wei, Donglu, Yizhuo Gu, Hanrui Zhu, Min Li, and Shaokai Wang. "Influence of Electrical Heating Metal Mesh and Power Density on Resistance Welding of Carbon Fiber/PEEK Composite." Polymers 14, no. 13 (2022): 2563. http://dx.doi.org/10.3390/polym14132563.

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An experimental investigation on the resistance welding of carbon-fiber-reinforced polyetheretherketone (PEEK) composite laminate using three types of stainless steel (SS) meshes with different sizes and electrical resistances as heating elements is reported. The objective of this study is to determine the influence of the metal mesh on the welding process and performance at different power densities ranging from 29 to 82 kW/m2. Resistance welding equipment is used to monitor the temperature and displacement along the thickness of the laminate. The results show that the power density determine

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Zhang, Ya Hui, Ji Hong Zhu, Jun Shuo Li, and Wei Hong Zhang. "Structural Optimization Design of an Aircraft Metal-Composite Wing." Applied Mechanics and Materials 341-342 (July 2013): 519–23. http://dx.doi.org/10.4028/www.scientific.net/amm.341-342.519.

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The problem of metal-composite wing structural optimization is discussed and a strategy is presented. Topology optimization method is applied to provide load transferring path of structure for concept design. Size, shape and other optimization method are used to provide detailed design for individual components. A three-phase optimization method is discussed for fiber reinforced composite laminate skin. Optimal parameters include ply angle, percentage, thickness, layer shape and sequence. The design of laminate for ease of manufacture is based on a set of manufacturing constraints. This paper

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Nestler, Daisy, Heike Jung, Maik Trautmann, et al. "New Sandwich Structures Consisting of Aluminium Foam and Thermoplastic Hybrid Laminate Top Layers." Materials Science Forum 825-826 (July 2015): 797–805. http://dx.doi.org/10.4028/www.scientific.net/msf.825-826.797.

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Sandwich structures consist of one light core layer and two top layers, which form the load-bearing structure. These layers have to be stiff and strong and have to protect the structure against indentations. The main task of the core layer is to keep the top layers in place and to generate a high shear stiffness. In order to obtain the required space between the top layers, the core layer has to have a high specific volume. Different sandwich materials with aluminium or steel top layers and cores of aluminium combs, corrugated aluminium sheets or aluminium foams are already known. In order to

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