Relevant bibliographies by topics / Metal matrix composite

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Metal matrix composite'

Author: Grafiati
Published: 4 June 2021
Last updated: 16 June 2025

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Journal articles on the topic "Metal matrix composite"

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Yang, Hui, Ming Chang, and Chunjing Wu. "Continuous Casting Preparation Process of Helical Fiber-Reinforced Metal Matrix Composites." Metals 14, no. 7 (2024): 832. http://dx.doi.org/10.3390/met14070832.

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To improve the strength of the metal while maintaining good plasticity, helical fibers are added to the metal matrix. How to form helical fiber and control its parameters in the preparation process are urgent problems to be solved in the study of helical fiber-reinforced metal matrix composites. In this paper, the continuous casting process of helical fiber-reinforced metal matrix composites was proposed. To reduce the difficulty of the experiment, the formation process of helical fiber on metal matrix and the relationship between the continuous casting process parameters and helical shape fiber parameters were studied by preparing helical carbon fiber-reinforced lead matrix composites with a low-melting-point metal matrix. The results show that this process can produce helical fiber-reinforced metal matrix composite stably and continuously, and the helical shape parameters of the composite can be controlled by changing the process parameters of continuous casting. To further improve the practical application of this process, helical carbon fiber-reinforced aluminum matrix composites were prepared. The test result in terms of mechanical property shows that the tensile strength and elongation of the composite were improved. This indicates that the reinforced phase of the helical structure of the metal matrix composite has higher strength and toughness compared with the matrix metal.
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Muribwathoho, Oritonda, Velaphi Msomi, and Sipokazi Mabuwa. "Metal Matrix Composite Fabricated with 5000 Series Marine Grades of Aluminium Using FSP Technique: State of the Art Review." Applied Sciences 12, no. 24 (2022): 12832. http://dx.doi.org/10.3390/app122412832.

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Aluminium metal matrix composites have been shown to make significant contributions to the area of new materials and have become widely accepted in high-tech structural and functional applications such as those in the aircraft, automobile, marine, mineral, defence, transportation, thermal management, automotive, and sports and recreation fields. Metal matrix composites are manufactured using a variety of manufacturing processes. Stirring casting, powder metallurgy, squeezing casting, in situ processes, deposition techniques, and electroplating are part of the manufacturing process used in the manufacture of aluminium-metal matrix composites. Metal matrix composites that use friction stir processing have a distinct advantage over metal matrix composites that use other manufacturing techniques. FSP’s benefits include a finer grain, processing zone homogeneity, densification, and the homogenization of aluminium alloy and composite precipitates. Most metal matrix composite investigations achieve aluminium-metal matrix composite precipitate grain refinement, treated zone homogeneity, densification, and homogenization. This part of the work examines the impact of reinforcing particles, process parameters, multiple passes, and active cooling on mechanical properties during the fabrication of 5000-series aluminium-metal matrix composites using friction stir processing. This paper reports on the available literature on aluminium metal matrix composites fabricated with 5xxx series marine grade aluminium alloy using FSP.
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Nurlan Gurbanov, Yusif Tanriverdiyev, Nurlan Gurbanov, Yusif Tanriverdiyev. "METAL MATRIX HYBRID LAYERED COMPOSITE MATERIALS." PAHTEI-Procedings of Azerbaijan High Technical Educational Institutions 46, no. 11 (2024): 284–90. https://doi.org/10.36962/pahtei46112024-31.

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Reducing the weight of components is a key goal in different industrial sectors. This leads to an increase in the application areas of fiber composites for primary structural components. Aiming at this goal, a new lightweight fiber-metal laminate composites have been developed. Fiber-metal laminate composites are one of such materials that have been widely investigated for their performance compared to existing materials. Depending on the type of matrix and fiber materials used in the industry, various types of fiber-metal laminate composites are available. In this article, the properties of these materials are examined in detail. Keywords: Composite materials, ARALL, GLARE, CARALL
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Bagali, Pavan Balappa. "Manufacturing of Aluminium Metal Matrix Composite after Critical Study." International Journal of Psychosocial Rehabilitation 24, no. 4 (2020): 5763–68. http://dx.doi.org/10.37200/ijpr/v24i4/pr2020381.

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Malaki, Massoud, Wenwu Xu, Ashish Kasar, et al. "Advanced Metal Matrix Nanocomposites." Metals 9, no. 3 (2019): 330. http://dx.doi.org/10.3390/met9030330.

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Lightweight high-strength metal matrix nano-composites (MMNCs) can be used in a wide variety of applications, e.g., aerospace, automotive, and biomedical engineering, owing to their sustainability, increased specific strength/stiffness, enhanced elevated temperature strength, improved wear, or corrosion resistance. A metallic matrix, commonly comprising of light aluminum or magnesium alloys, can be significantly strengthened even by very low weight fractions (~1 wt%) of well-dispersed nanoparticles. This review discusses the recent advancements in the fabrication of metal matrix nanocomposites starting with manufacturing routes and different nanoparticles, intricacies of the underlying physics, and the mechanisms of particle dispersion in a particle-metal composite system. Thereafter, the microstructural influences of the nanoparticles on the composite system are outlined and the theory of the strengthening mechanisms is also explained. Finally, microstructural, mechanical, and tribological properties of the selected MMNCs are discussed as well.
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Yadav, Govind, R. S. Rana, R. K. Dwivedi, and Ankur Tiwari. "Development and Analysis of Automotive Component Using Aluminium Alloy Nano Silicon Carbide Composite." Applied Mechanics and Materials 813-814 (November 2015): 257–62. http://dx.doi.org/10.4028/www.scientific.net/amm.813-814.257.

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Composite materials are important engineering materials due to their outstanding mechanical properties. Composites are materials in which the desirable properties of separate materials are combined by mechanically binding them together. Each of the components retains its structure and characteristic, but the composite generally possesses better properties. Composite materials offer superior properties to conventional alloys for various applications as they have high stiffness, strength and wear resistance. The development of these materials started with the production of continuous-fiber-reinforced composites. The high cost and difficulty of processing these composites restricted their application and led to the development of discontinuously reinforced composites. The aim involved in designing metal matrix composite materials is to combine the desirable attributes of metals and ceramics. The addition of high strength, high modulus refractory particles to a ductile metal matrix produce a material whose mechanical properties are intermediate between the matrix alloy and the ceramic reinforcement. Metal Matrix Composites with Aluminum as metal matrix is the burning area for research now a days.
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Nandakumar, A., and D. Dinakaran. "Effect of Nanoparticles in Reinforced Metal Matrix Composite on the Machinability Characteristics - A Review." Applied Mechanics and Materials 813-814 (November 2015): 625–28. http://dx.doi.org/10.4028/www.scientific.net/amm.813-814.625.

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Metal Matrix nanoComposites (MMNC) refer to materials consisting of a ductile metal or alloy matrix in which some nanosized reinforcement materials is implanted. These materials combine metal and ceramic features, i.e., ductility and toughness with high strength. Thus, metal matrix nanocomposites are suitable for production of materials with high strength in shear/compression processes and high service temperature capabilities. Both Metal Matrix Composite (MMC) and Ceramic Matrix Composites (CMC) with Carbon nanoTubes (CNT) nanocomposites hold promise, but also pose challenges for real success. In the present paper deals an inclusive review of literature in effect of nanoparticles in reinforced metal matrix composites on the machinability characteristics of the composite materials.
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Burke, M. G., M. N. Gungor, and P. K. Liaw. "TEM examination of 2014-SiC metal matrix composite." Proceedings, annual meeting, Electron Microscopy Society of America 46 (1988): 726–27. http://dx.doi.org/10.1017/s0424820100105692.

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Aluminum-based metal matrix composites offer unique combinations of high specific strength and high stiffness. The improvement in strength and stiffness is related to the particulate reinforcement and the particular matrix alloy chosen. In this way, the metal matrix composite can be tailored for specific materials applications. The microstructural characterization of metal matrix composites is thus important in the development of these materials. In this study, the structure of a p/m 2014-SiC particulate metal matrix composite has been examined after extrusion and tensile deformation.Thin-foil specimens of the 2014-20 vol.% SiCp metal matrix composite were prepared by dimpling to approximately 35 μm prior to ion-milling using a Gatan Dual Ion Mill equipped with a cold stage. These samples were then examined in a Philips 400T TEM/STEM operated at 120 kV. Two material conditions were evaluated: after extrusion (80:1); and after tensile deformation at 250°C.
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Singh, Lokesh, Shankar Sehgal, and K. Saxena Kuldeep. "Behaviour of Al2O3 in aluminium matrix composites: An overview." E3S Web of Conferences 309 (2021): 01028. http://dx.doi.org/10.1051/e3sconf/202130901028.

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In this paper, behaviour of Al2O3 in aluminium matrix composites is reviewed for its properties and applications. In addition, many metal matrix composite fabrication processes are also elaborated. In the present days the aluminium metal matrix composite is in high demand because of its superior properties. Its demand is still on rise because of its widespread use in automotive industries, aerospace industries and marine industries. The method of the fabrication of aluminium matrix-based composite is also a deciding factor for its resultant properties. Desired composite-properties are achievable by proper selection of reinforcing materials as well as the physical conditions. Various sections of current information compile the details about the behaviour of alumina particles in aluminium-based matrix for formation of metal matrix composites.
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Moreira, Roberta Cristina Silva, Oksana Kovalenko, Daniel Souza, and Ruham Pablo Reis. "Metal matrix composite material reinforced with metal wire and produced with gas metal arc welding." Journal of Composite Materials 53, no. 28-30 (2019): 4411–26. http://dx.doi.org/10.1177/0021998319857920.

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In the search for high-performance parts and structures, especially for the aviation and aerospace industry, metal matrix composites appear with prominence. However, despite exhibiting high levels of mechanical properties and low densities, these materials are still very expensive, mainly due to complex production. Thus, this work aims to present and evaluate a novel way of manufacturing metal matrix composites, with relative low cost and complexity: by using low-energy fusion welding to deposit the matrix material on top of continuous metal wire reinforcement. For proof of concept, Al alloy was used as matrix material, a single Ti alloy wire as reinforcement, and gas metal arc welding CMT-Pulse® as the process for material deposition. The simplified Al–Ti composite was evaluated in terms of impact resistance and tensile strength and stiffness. Overall, the mechanical performance of the composite was around 23% higher than that of the matrix material itself (Al), this with only about 2% of reinforcement volume and just over 3% of increase in weight. Analyses of the Al–Ti composite fractures and cross-sections and of chemical composition and hardness of the matrix–reinforcement transition interface indicated the preservation (no melting) of the Ti wire and the existence of a fine contour of bonding between matrix and reinforcement. At the end, a brief discussion on the dynamics of the wire reinforcement preservation is carried out based on high-speed filming.
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Dissertations / Theses on the topic "Metal matrix composite"

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Otani, T. "Corrosion behaviour of metal matrix composite." Thesis, University of Bath, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.382471.

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DONNINI, RICCARDO. "Metal matrix composite: structure and technologies." Doctoral thesis, Università degli Studi di Roma "Tor Vergata", 2009. http://hdl.handle.net/2108/868.

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I compositi a matrice metallica sono materiali aventi elevate potenzialità di applicazione, i cui punti critici riguardano soprattutto le tecnologie di produzione e le lavorazioni alle macchine utensili. Un composito a matrice di titanio rinforzato con lunghe fibre unidirezionali in SiC, il Ti6Al4V-SiCf, è candidato per componenti di turbine aeronautiche soggette a medie temperature (fino a 600°C) per lunghi tempi di esposizione. Per questo ne sono state esaminate sia le reazioni di tipo microchimico, le quali accadono soprattutto nell’interfaccia fibra/matrice, sia le proprietà meccaniche. La microstruttura allo stato tal quale e dopo lunghi trattamenti termici (fino a 100 ore e 600°C) è stata esaminata mediante diffrazione ai raggi X (XRD), spettrometria elettronica (SEM/EDS), spettroscopia di fotoemissione (XPS) e spettroscopia Auger (AES). Il comportamento meccanico, anche qui sia allo stato tal quale che dopo trattamenti termici, è stato studiato attraverso prove ad indentazione strumentata (FIMEC), di modulo dinamico, prove di trazione e di fatica. Inoltre sono state eseguite prove di frizione interna per verificare il caratteristico comportamento anelastico del materiale, durante condizioni di elevato stato vibrazionale e di alta temperatura. Lo studio, sviluppato sullo stesso composito prodotto però mediante due processi di fabbricazione differenti come Hot Isostatic Pressure and Roll Diffusion Bonding, ha confermato l’idoneità del materiale alle applicazioni considerate. Per quanto riguarda lo studio della lavorabilità, sono stati studiati, dal punto di vista dell’operazione di foratura, i materiali compositi a matrice di alluminio rinforzati a fibre corte o particolato, valutando le migliori condizioni di riduzione delle forze di taglio, soprattutto in funzione delle temperatura del pezzo da forare.<br>Metal matrix composites are materials having high application potentiality, whose critical points regards especially production technology and machining. A titanium matrix composite reinforced by unidirectional SiC fibers, Ti6Al4V-SiCf , is candidate to components of aeronautical turbines subjected at middle temperatures (500-600°C) for long exposure time. It has been examined about the micro-chemical reactions, occurring especially on the fiber-matrix interface, and the mechanical properties. The microstructure, in as-fabricated condition and after long-term heat treatments simulating the work condition has been investigated by means of high-temperature X-ray diffraction (XRD), energy dispersion spectrometry (SEM/EDS), X-ray photoelectron spectroscopy (XPS) and Auger electron spectroscopy (AES). The mechanical behaviour, in as-fabricated condition and after heat treatments, have been inspected by instrumented indentation (FIMEC), dynamic modulus, tensile and fatigue tests. Moreover, to the verify the characteristic anelastic phenomena for the composite, internal friction probes have been carried out by using a vibrating reed technique with electrostatic excitation and frequency modulation detection of flexural vibration. The study has been developed on the same composite produced by two different fabrication process, Hot Isostatic Pressure and Roll Diffusion Bonding, confirming the suitable of the material for the considered applications. About the composite machining, aluminium matrix composite reinforced by short fiber or particle has been studied about drilling operations, evaluating the better condition to reduce the cutting forces (thrust and torque), especially as function of the workpiece temperature (hot drilling)
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Ward, William F. "A theoretical investigation into the inelastic behavior of metal-matrix composites." Thesis, Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/17244.

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Ellerby, Donald Thomas. "Processing and mechanical properties of metal-ceramic composites with controlled microstructure formed by reactive metal penetration /." Thesis, Connect to this title online; UW restricted, 1999. http://hdl.handle.net/1773/10583.

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Abdullah, Abu. "Machining of aluminium based Metal Matrix Composite (MMC)." Thesis, University of Warwick, 1996. http://wrap.warwick.ac.uk/34661/.

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The machining of aluminium 2618 particulate reinforced Metal Matrix Composite (MMC) with 18 vol. % silicon carbide (SiC) using cemented carbide cutting tools has been undertaken. Two grades of cemented carbide inserts, uncoated K68 grade and coated KC910 grade (coated with TiC and A1203) having negative and positive rake angles (with and without chip breaker) have been used to machine this material in order to understand the machining process, tool failure modes and wear mechanisms. Turning tests in the speed range 15 - 10 m/min have been carried out at 0.2,0.4 and 0.6 mm/rev feed rates and 2 mm and 4 mm depths of cut. Both cemented carbide tools have been shown to be capable of machining the MMC and give reasonable tool lives. Low speed and high feed rate are found to be a good combination in order to machine this material effectively. Coated KC910 grade inserts with negative rake angle gave the best performance. The use of a chip breaker has no significant effect on the machining process of the NMC because the material is one which inherently short chips due to ductility limitations caused by the particles. Tool failure mode studies showed that the tools failed by flank wear. Tool wear mechanism analysis indicated that abrasion wear was the tool life controlling factor under all cutting conditions. The tool wear is related to the direct contact between the abrasive hard SiC particles and the cutting edge and their relative motion to the rake and clearance face. Hence, the hardness of the SiC particles is a dominant factor for the tool wear. Two separatem odels of abrasio. n haye.b een suggested.B uilt-up edge (BUE) which has a distinct shape was more pro i1ounced at lower cutting speeds, high feed rates and greater depth of cut. The presence of BUE has been found to increase tool life and reduce tool wear but at the expense of surface finish. The increase in tool life or reduction in tool wear is likely due to the protective layer that the BUE formed on the tool surface preventing a direct contact between the tool and chip. Linear regression analysis showed that the value of Taylor exponent n is high (0.8-1.0) compared to the values of n (0.2-0.3) obtained when machining steel. This indicates that the tool life is less sensitive to cutting speed for MMC than it is for steel.
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Drury, William James. "Quantitative microstructural and fractographic characterization of AE-Li/FP metal matrix composite." Thesis, Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/19958.

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Arenburg, Robert Thomas. "Analysis of metal matrix composite structures using a micromechanical constitutive theory." Diss., Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/49918.

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The nonlinear behavior of continuous-fiber-reinforced metal-matrix composite structures is examined using a micromechanical constitutive theory. Effective lamina and laminate constitutive relations based on the Aboudi micromechanics theory are presented. The inelastic matrix behavior is modeled by the unified viscoplasticity theory of Bodner and Partom. The laminate constitutive relations are incorporated into a first-order shear deformation plate theory. The resulting boundary value problem is solved by utilizing the finite element method. · Computational aspects of the numerical solution, such as the temporal integration of the inelastic strains and the spatial integration of bending moments are addressed. Numerical results are presented which illustrate the nonlinear response of metal matrix composites subjected to extensional and bending loads. Experimental data from available literature are in good agreement with the numerical results.<br>Ph. D.<br>incomplete_metadata
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Huang, Ching-Yao. "Applications of Pressure Cycling on Metal Matrix Composite Processing /." The Ohio State University, 1996. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487933648651449.

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Clews, Justin David. "Ultrasonic consolidation of continuous fiber metal matrix composite tape." Access to citation, abstract and download form provided by ProQuest Information and Learning Company; downloadable PDF file, 190 p, 2009. http://proquest.umi.com/pqdweb?did=1885474451&sid=1&Fmt=2&clientId=8331&RQT=309&VName=PQD.

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Franklin, Jennifer. "In-situ Synthesis of Piezoelectric-Reinforced Metal Matrix Composites." Thesis, Virginia Tech, 2001. http://hdl.handle.net/10919/10141.

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The in-situ synthesis of piezoelectric-reinforced metal matrix composites has been attempted with a variety of target matrix and reinforcement materials using reaction synthesis and high energy ball milling. Zinc oxide (ZnO) and barium titanate (BaTiO₃) have been successfully synthesized within copper and iron matrices in a range of volume percentages using reaction synthesis. The microstructures of these composites have been analyzed and found to partially consist of an interpenetrating microstructure. After considering experimental findings and thermodynamic issues involved with synthesis, ideal reaction system parameters have been identified that promote the creation of a composite with ideal microstructure and formulated composition. Reactive high energy ball milling has been used to create copper matrix composites reinforced with zinc oxide and copper matrix composites reinforced with lead titanate (PbTiO₃). The microstructures and compositions of each volume percentage formulation of the composite powders have been analyzed. In this work, several promising piezoelectric-reinforced metal matrix composite systems have been identified as having potential to be synthesized in an in-situ manner.<br>Master of Science
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Books on the topic "Metal matrix composite"

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(Firm), Knovel, ed. Composite materials handbook: Metal matrix composites. U.S. Department of Defense, 2002.

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Engineers, Society of Automotive, and International Congress and Exposition (1994 : Detroit, Mich.), eds. Metal matrix composites. Society of Automobile Engineers, 1994.

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Stephens, Joseph R. High temperature metal matrix composites for future aerospace systems. National Aeronautics and Space Administration, 1987.

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Johnson, W. S. Fatigue damage accumulation in various metal matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1987.

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Davim, J. Paulo. Machining of Metal Matrix Composites. Springer-Verlag London Limited, 2012.

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Bryant, Richard W. Metal matrix composites: New developments, applications, and markets. Business Communications Co., 1988.

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Morel, M. Concurrent micromechanical tailoring and fabrication process optimization for metal-matrix composites. National Aeronautics and Space Administration, 1991.

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Roux, Teresa Le. The machining of a metal matrix composite. University of Birmingham, 1994.

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J, Lee H., and United States. National Aeronautics and Space Administration., eds. Metal matrix composite analyzer: METCAN user's manual. 4th ed. National Aeronautics and Space Administration, 1991.

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C, Chamis C., and United States. National Aeronautics and Space Administration., eds. METal matrix Composite ANalyzer (METCAN): Theoretical manual. National Aeronautics and Space Administration, 1993.

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Book chapters on the topic "Metal matrix composite"

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Chawla, Krishan K. "Metal Matrix Composites." In Composite Materials. Springer New York, 2012. http://dx.doi.org/10.1007/978-0-387-74365-3_6.

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Chawla, Krishan K. "Metal Matrix Composites." In Composite Materials. Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4757-2966-5_6.

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Chawla, Krishan Kumar. "Metal Matrix Composites." In Composite Materials. Springer New York, 1987. http://dx.doi.org/10.1007/978-1-4757-3912-1_6.

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Chawla, Krishan K. "Metal Matrix Composites." In Composite Materials. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-28983-6_6.

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Geng, Lin, and Kun Wu. "Metal Matrix Composites." In Composite Materials Engineering, Volume 2. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-5690-1_3.

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Kishkina, S. I. "Mechanical testing of composite materials." In Metal Matrix Composites. Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-1266-6_10.

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Tchubarov, V. M., A. A. Zabolotsky, and G. A. Krivov. "Metal matrix composite fabrication methods." In Metal Matrix Composites. Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-1266-6_3.

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Wong, Wai Leong Eugene, and Sankaranarayanan Seetharaman. "Metal Matrix Composites." In Advances in Machining of Composite Materials. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-71438-3_6.

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Gnanaraj, S. Darius, and T. Ram Prabhu. "Tribological Properties of Metal Matrix Composites." In Composite and Composite Coatings. CRC Press, 2022. http://dx.doi.org/10.1201/9781003109723-6.

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Blawert, C. "Noble and Nonferrous Metal Matrix Composite Materials." In Metal Matrix Composites. Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527608117.ch12.

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Conference papers on the topic "Metal matrix composite"

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Hansen, Bruce, Jason Fetty, Timothy Demers, and Treven Baker. "Aluminum Metal Matrix Composite Liner Testing." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10248.

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Bearing liners are used in rotorcraft gearboxes to reduce wear between the bearing race and housing during aircraft operations. Bearing liners are typically made of steel, but a new aluminum Metal Matrix Composite (MMC) bearing liner material is currently being developed under the Future Advanced Rotorcraft Drive System (FARDS) program. These new bearing liners have the benefit of reduced weight compared to existing steel liners. Seeded fault testing was performed which demonstrated the liners ability to withstand the loads generated due to failing bearings and still left the housing assembly in serviceable condition after removal. The test was in support of a viability study evaluating use of aluminum MMC liners for weight savings.
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Baliashvili, Giorgi, Sophiko Kvinikadze, Tamar Iashvili, Davit Tsverava, and Aleksandre Vanishvili. "DEVELOPMENT OF METAL-POLYMER LAMINATE WITH HIGH MECHANICAL PROPERTIES." In SGEM International Multidisciplinary Scientific GeoConference 24. STEF92 Technology, 2024. https://doi.org/10.5593/sgem2024/6.1/s24.04.

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Basalt fiber-reinforced metal-polymer composites represent a cutting-edge class of materials that merge the robustness of metal with the pliability of polymer. Originating from natural volcanic rocks, basalt fibers possess remarkable mechanical properties, such as high tensile strength, resistance to extreme temperatures, and chemical inertness. Integrating basalt fibers into a polymer matrix like epoxy or thermoplastic resins significantly boosts the composite's resistance to dynamic impacts and its energy absorption capacity. The metal component ensures structural integrity and strength, while the polymer matrix distributes energy through elastic deformation. Basalt fibers find application across various industries, including aviation, automotive, and military technology. There are research centers and scientific groups whose work is focused on developing polymer composite materials reinforced with basalt fibers. These metal-polymer composites are especially valuable for their application in an automotive industry, aerospace and construction, due to their high strength to weight ratio, as well as for the ability to absorb impact energy, flexibility in design and chemical resistance. The objective of this study is to develop a technology for producing basalt fiber-based metal-polymer composites and to investigate the physical and mechanical properties of these materials. Using Vacuum Infusion Process (VIP) technology, metal-polymer composites incorporating basalt fiber were produced. The resulting samples exhibit high bonding strength, uniform polymer distribution within the matrix, and a straightforward manufacturing process. Experimental samples of the metal-polymer composites, produced using VIP technology, were tested under mechanical and dynamic loads.
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NOVOTNÝ, Adam, Pavel ROHAN, Jakub KARMÁČEK, Miroslav SAHUL, and Marie KOLAŘÍKOVÁ. "Preparation and Basic Characteristics of Nickel Matrix Composite." In METAL 2024. TANGER Ltd., 2024. http://dx.doi.org/10.37904/metal.2024.4968.

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RAVENHALL, R., and W. KOOP. "Metal matrix composite fan blade development." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2178.

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HUANG, C. "Damage of Metal Matrix Composite Materials." In 31st Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1025.

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Mishra, Ashish, and Sivasambu Mahesh. "Reliability of Ti/SiC Metal Matrix Composites." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4859.

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Abstract:
Components such as bladed rings, and bladed disks fabiricated out of titanium matrix composites were extensively explored in the two decades since about 1990 as light weight replacements for conventional superalloy blades and disks in the intermediate hot stages of gas turbines. One of the challenges, which has hindered their adoption is the relative unreliability of the composite components; nominally identical Ti composite specimen display a much larger variability in strength than their superalloy counterparts. In the present work, we have quantified the reliability of Ti matrix composites by developing a detailed micromechanical-statistical model of their failure. The micromechanical model resolves fibres, matrix, and the interface, and accounts for such failure modes as fibre breakage, matrix cracking, matrix plasticity, interfacial sliding, and debonding. It also accounts for mechanical interaction between these various failure modes. The mechanical model’s predictions are validated against synchotron X-ray measurements reported in the literature, both after loading, and unloading. Using the detailed micromechanical model, Ti matrix composite was simulated following a Monte Carlo framework. These simulations yield the empirical strength distribution of the Ti matrix composite, and insights into the dominant failure mode. The latter allows the construction of a stochastic model of composite failure. The stochastic model can be used to determine safe working loads as a function of composite size for any desired reliability level.
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PELACHOVÁ, Tatiana, and Juraj LAPIN. "Fracture initiation and propagation in in-situ TiAl matrix composite reinforced with carbide particles." In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.751.

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KAMYSHNYKOVA, Kateryna, and Juraj LAPIN. "Microstructure optimisation of centrifugally cast in-situ TiAl-based matrix composite reinforced with Ti2AlC particles." In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.942.

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Johnson, R. Barry, Anees Ahmad, James B. Hadaway, and Alan L. Geiger. "Lightweight SXA® metal matrix composite collimator." In San Diego, '91, San Diego, CA, edited by Gary W. Wilkerson. SPIE, 1991. http://dx.doi.org/10.1117/12.48310.

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Ulph, Eric. "Fabrication Of A Metal-Matrix Composite Mirror." In 32nd Annual Technical Symposium, edited by Jones B. Arnold and Robert E. Parks. SPIE, 1989. http://dx.doi.org/10.1117/12.948056.

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Reports on the topic "Metal matrix composite"

1

Smith, Don D. Steel-SiC Metal Matrix Composite Development. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/967387.

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2

De Rosset, William S. Nondestructive Evaluation of a Metal Matrix Composite. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada419365.

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Lavender, C. A., and M. T. Smith. Evaluation of waterjet-machined metal matrix composite tensile specimens. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5754921.

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Wu, Yufeng. Fabrication of metal matrix composite by semi-solid powder processing. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1082974.

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Levoy, Nancy F. Ductile - Ductile Beryllium Aluminum Metal Matrix Composite Manufactured by Extrusion1. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada289519.

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Raja, Krishnan, and Ravi subramanian. COLD SPRAY COATED METAL MATRIX NANO-COMPOSITE SURFACE LAYERS ON INCONEL 617. Office of Scientific and Technical Information (OSTI), 2022. http://dx.doi.org/10.2172/1868153.

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Lee, H. R., W. Yun, Z. Cai, W. Rodrigues, and D. S. Kupperman. X-ray microdiffraction studies to measure strain fields in a metal matrix composite. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/555507.

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Howell, Paul R. Microstructural Development in a Spray Formed Aluminum-Silicon Carbide Based Metal Matrix Composite. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada251425.

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Kumar, Ramasamy Sanjeev, Allaka Gopichand, and Rajumani Srinivasan. Fabrication, Microstructural and Mechanical Behaviour of Al-ZrO2 -TiC Hybrid Metal Matrix Composite. "Prof. Marin Drinov" Publishing House of Bulgarian Academy of Sciences, 2021. http://dx.doi.org/10.7546/crabs.2021.11.10.

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Altshuler, Thomas L. Tensile Tests for Various Specimen Configurations for Metal Matrix Composite P55 GR/AL 6061-T6. Defense Technical Information Center, 1988. http://dx.doi.org/10.21236/ada220747.

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