Academic literature on the topic 'Metal matrix composites'

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Journal articles on the topic "Metal matrix composites"

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Kosnikov, Gennadiy, Oleg Figovsky, and Adnan Eldarkhanov. "Metal Matrix Micro- and Nanostructural Composites (Review)." Chemistry & Chemical Technology 9, no. 2 (2015): 165–70. http://dx.doi.org/10.23939/chcht09.02.165.

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K, Nithin. "Characterization of AlWCFly ash Metal Matrix Composites." International Journal of Trend in Scientific Research and Development Volume-2, Issue-3 (2018): 465–70. http://dx.doi.org/10.31142/ijtsrd10937.

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J., Leela Krishna. "Applications of Magnesium Metal Matrix Composites-A Review." Journal of Advanced Research in Dynamical and Control Systems 12, SP3 (2020): 10–16. http://dx.doi.org/10.5373/jardcs/v12sp3/20201232.

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Karumuri, Srikanth. "Mechanical Behaviour of Metal Matrix Composites - A Review." Journal of Advanced Research in Dynamical and Control Systems 12, SP7 (2020): 1042–49. http://dx.doi.org/10.5373/jardcs/v12sp7/20202201.

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Gupta, Manoj. "Metal Matrix Composites." Metals 8, no. 6 (2018): 379. http://dx.doi.org/10.3390/met8060379.

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Rohatgi, Pradeep K. "Metal matrix Composites." Defence Science Journal 43, no. 4 (1993): 323–49. http://dx.doi.org/10.14429/dsj.43.4336.

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Morita, Mikio. "Metal matrix composites." Advanced Composite Materials 4, no. 3 (1995): 237–46. http://dx.doi.org/10.1163/156855195x00041.

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Mortensen, Andreas, and Javier Llorca. "Metal Matrix Composites." Annual Review of Materials Research 40, no. 1 (2010): 243–70. http://dx.doi.org/10.1146/annurev-matsci-070909-104511.

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Bryant, Richard. "Metal Matrix Composites." Materials and Processing Report 3, no. 9 (1988): 4–6. http://dx.doi.org/10.1080/08871949.1988.11752216.

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Harris, S. J. "Metal matrix composites." Composites Science and Technology 35, no. 2 (1989): 99–103. http://dx.doi.org/10.1016/0266-3538(89)90090-0.

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Dissertations / Theses on the topic "Metal matrix composites"

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Ling, Paul Keh Yiing. "Creep of metal matrix composites." Thesis, University of Nottingham, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.240496.

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Zwigl, Peter 1963. "Transformation-superplasticity of metals and metal matrix composites." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/49665.

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Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Materials Science and Engineering, 1998.<br>Includes bibliographical references (p. 156-162).<br>The work covers transformation superplasticity of metals, alloys and metal matrix composites. Fundamental studies of transformation superplasticity in unreinforced metals, which either deform plastically or by creep, form the basis of further investigations in metal matrix composites. Experiments and analytical modeling are complemented by numerical analysis. The transformation superplastic behavior is related to microstructure and chemical composition. Based on an existing linear theory, a non-linear model is developed and applied to the experimental data. Numerical methods are used to model the stress-, strain and temperature evolution during the phase transformation. The results are in good agreement with the experiment and analytical predictions. First, transformation superplasticity of iron and iron-TiC composites is demonstrated with strains of 450% and 230% respectively. The reduction of the transformation superplasticity in the composites is attributed to the dissolution of TiC in iron and effect which is shown for iron-carbon alloys. Effects of transient primary creep, ratchetting and partial transformation through the ferrite-austenite phase field are examined. Second, transformation superplasticity of zirconium is demonstrated for the first time with a strain of 270% without fracture. Partial transformation resulting from high cycle frequencies is analyzed and related to material properties and cycle characteristics. Finally, nickel aluminide with unstabilized zirconia particulates shows significant higher strain rates upon thermal cycling as compared to the unreinforced matrix. Although, the fracture strain of 23% is below the superplastic limit, the composite shows a high strain rate sensitivity of m = 0.71, which is a necessary characteristic of transformation superplasticity.<br>by Peter Zwigl.<br>Ph.D.
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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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Schuler, Sabine. "Modelling consolidation of matrix-coated fibre metal matrix composites." Thesis, University of Oxford, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.284419.

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El-Gallab, Mariam S. "Machining of particulate metal matrix composites." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape8/PQDD_0030/NQ66206.pdf.

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Murphy, Angela Mary. "Clustering in particulate metal matrix composites." Thesis, University of Cambridge, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.242540.

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Wildan, Muhammad W. "Zirconia-matrix composites reinforced with metal." Thesis, University of Strathclyde, 2000. http://oleg.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=21428.

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The aim of this study was to investigate a zirconia-matrix reinforced with metal powder (chromium, iron and stainless steel (AISI 316)) including processing, characterisation, and measurements of their properties (mechanical, thermal and electrical). Zirconia stabilised with 5.4 wt% Y₂0₃ (3 mol%) as the matrix was first studied and followed by an investigation of the effects of metal reinforcement on zirconia-matrix composites. Monolithic zirconia was pressureless sintered in air and argon to observe the effect of sintering atmosphere, while the composites were pressureless sintered in argon to avoid oxidation. Sintering was carried out at various temperatures for 1 hour and 1450°C was chosen to get almost fully dense samples. The density of the fired samples was measured using a mercury balance method and the densification behaviour was analysed using TMA (Thermo-mechanical Analysis). The TMA was also used to measure the coefficient of thermal expansion. In addition, thermal analysis using DTA and TGA was performed to observe reactions and phase transformations. Moreover, optical microscopy and SEM were used to observe the microstructures, XRD was used for phase identification, and mechanical properties including Vickers hardness, fracture toughness and bending strength were measured. The effect of thermal expansion mismatch on thermal stresses was also analysed and discussed. Finally, thermal diffusivity at room temperature and as a function of temperature was measured using a laser flash method, and to complete the study, electrical conductivity at room temperature was also measured. The investigation of monolithic zirconia showed that there was no significant effect of air and argon atmosphere during sintering on density, densification behaviour, microstructures, and properties (mechanical and thermal). Furthermore, the results were in good agreement with that reported by previous researchers. However, the presence of metal in the composites influenced the sintering behaviour and the densification process depends on the metal stability, reactivity, impurity, particle size, and volume fraction. Iron reacted with yttria (zirconia stabiliser), melted and reduced the densification temperature of monolithic zirconia, while chromium and AISI 316 did not significantly affect the densification temperature and did not react with either zirconia or yttria. AISI 316 melted during fabrication. Moreover, all of the metal reinforcements reduced the final shrinkage of monolithic zirconia. In terms of properties, the composites showed an increase in fracture toughness, and a reduction in Vickers hardness and strength with increasing reinforcement content. In addition, the thermal diffusivity of the composites showed an increase with reinforcement content for the zirconia/chromium and zirconia/iron composites, but not for the zirconia/AISI 316 composites due to intrinsic mircocracking. Furthermore, all the composites became electrically conductive with 20 vol% or more of reinforcement. It has been concluded that of those composites the zirconia/chromium system may be considered as having the best combination of properties and although further development is needed for such composites to be used in real applications in structural engineering, the materials may be developed based on these findings. In addition, these findings may be used in development of ceramic/metal joining as composite interlayers are frequently used.
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Mohammadi-Aghdam, Mohammad. "Micromechanics of unidirectional metal matrix composites." Thesis, University of Bristol, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297843.

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Wang, Aiguo. "Abrasive wear of metal matrix composites." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305516.

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Dibelka, Jessica Anne. "Mechanics of Hybrid Metal Matrix Composites." Diss., Virginia Tech, 2013. http://hdl.handle.net/10919/50579.

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The appeal of hybrid composites is the ability to create materials with properties which normally do not coexist such as high specific strength, stiffness, and toughness. One possible application for hybrid composites is as backplate materials in layered armor. Fiber reinforced composites have been used as backplate materials due to their potential to absorb more energy than monolithic materials at similar to lower weights through microfragmentation of the fiber, matrix, and fiber-matrix interface. Composite backplates are traditionally constructed from graphite or glass fiber reinforced epoxy composites. However, continuous alumina fiber-reinforced aluminum metal matrix composites (MMCs) have superior specific transverse and specific shear properties than epoxy composites. Unlike the epoxy composites, MMCs have the ability to absorb additional energy through plastic deformation of the metal matrix. Although, these enhanced properties may make continuous alumina reinforced MMCs advantageous for use as backplate materials, they still exhibit a low failure strain and therefore have low toughness. One possible solution to improve their energy absorption capabilities while maintaining the high specific stiffness and strength properties of continuous reinforced MMCs is through hybridization. To increase the strain to failure and energy absorption capability of a continuous alumina reinforced Nextel" MMC, it is laminated with a high failure strain Saffil® discontinuous alumina fiber layer. Uniaxial tensile testing of hybrid composites with varying Nextel" to Saffil® reinforcement ratios resulted in composites with non-catastrophic tensile failures and an increased strain to failure than the single reinforcement Nextel" MMC. The tensile behavior of six hybrid continuous and discontinuous alumina fiber reinforced MMCs are reported, as well as a description of the mechanics behind their unique behavior. Additionally, a study on the effects of fiber damage induced during processing is performed to obtain accurate as-processed fiber properties and improve single reinforced laminate strength predictions. A stochastic damage evolution model is used to predict failure of the continuous Nextel" fabric composite which is then applied to a finite element model to predict the progressive failure of two of the hybrid laminates.<br>Ph. D.
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Books on the topic "Metal matrix composites"

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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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Srivatsan, T. S., Pradeep K. Rohatgi, and Simona Hunyadi Murph, eds. Metal-Matrix Composites. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-92567-3.

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Bansal, Suneev Anil, Virat Khanna, and Pallav Gupta. Metal Matrix Composites. CRC Press, 2022. http://dx.doi.org/10.1201/9781003194910.

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Bansal, Suneev Anil, Virat Khanna, and Pallav Gupta. Metal Matrix Composites. CRC Press, 2022. http://dx.doi.org/10.1201/9781003194897.

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Natarajan, Nanjappan, Vijayan Krishnaraj, and J. Paulo Davim. Metal Matrix Composites. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-02985-6.

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Davim, J. Paulo, ed. Metal Matrix Composites. DE GRUYTER, 2014. http://dx.doi.org/10.1515/9783110315448.

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Contreras Cuevas, Antonio, Egberto Bedolla Becerril, Melchor Salazar Martínez, and José Lemus Ruiz. Metal Matrix Composites. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-91854-9.

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Fridlyander, J. N., ed. Metal Matrix Composites. Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-1266-6.

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Gieskes, Sebastiaan A., and Marten Terpstra, eds. Metal Matrix Composites. Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3666-2.

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Chawla, Nikhilesh, and Krishan K. Chawla. Metal Matrix Composites. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-9548-2.

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Book chapters on the topic "Metal matrix composites"

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Chawla, Nikhilesh, and Krishan K. Chawla. "Matrix Materials." In Metal Matrix Composites. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-9548-2_3.

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Mittal, Prateek, Jimmy Mehta, Seema Mahto, and Sahil Mehta. "Copper Matrix Composites." In Metal Matrix Composites. CRC Press, 2022. http://dx.doi.org/10.1201/9781003194897-3.

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Kobayashi, Toshiro. "Metal Matrix Composites." In Strength and Toughness of Materials. Springer Japan, 2004. http://dx.doi.org/10.1007/978-4-431-53973-5_8.

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de Cortázar, Maider García, Pedro Egizabal, Jorge Barcena, and Yann Le Petitcorps. "Metal Matrix Composites." In Structural Materials and Processes in Transportation. Wiley-VCH Verlag GmbH & Co. KGaA, 2013. http://dx.doi.org/10.1002/9783527649846.ch9.

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Kostikov, V. I., and V. S. Kilin. "Metal Matrix Composites." In Handbook of Composites. Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-6389-1_14.

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Hihara, L. H. "Metal-Matrix Composites." In Uhlig's Corrosion Handbook. John Wiley & Sons, Inc., 2011. http://dx.doi.org/10.1002/9780470872864.ch35.

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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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Kishawy, Hossam A., and Ali Hosseini. "Metal Matrix Composites." In Materials Forming, Machining and Tribology. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-95966-5_5.

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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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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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Conference papers on the topic "Metal matrix composites"

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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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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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LAPIN, Juraj. "Cast in-situ TiAl-based matrix composites reinforced with carbide particles." In METAL 2019. TANGER Ltd., 2019. http://dx.doi.org/10.37904/metal.2019.747.

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PRUSOV, Evgeny, Vladislav DEEV, and Vladimir KECHIN. "Selection of Reinforcing Phases for Aluminum Matrix Composites Using Thermodynamic Stability Criterion." In METAL 2020. TANGER Ltd., 2020. http://dx.doi.org/10.37904/metal.2020.3609.

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Jacobsen, Ronald L. "High Thermal Conductivity Metal Matrix Composites." In Aerospace Power Systems Conference. SAE International, 1999. http://dx.doi.org/10.4271/1999-01-1358.

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KOOP, W., and C. CROSS. "Metal matrix composites structural design experience." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2175.

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Hashiguchi, Don H., David Tricker, and Andrew D. Tarrant. "Mechanically alloyed aluminum metal matrix composites." In Material Technologies and Applications to Optics, Structures, Components, and Sub-Systems III, edited by Joseph L. Robichaud, Bill A. Goodman, and Matthias Krödel. SPIE, 2017. http://dx.doi.org/10.1117/12.2272421.

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Sundar, G., and N. Rajesh Jesudoss Hynes. "Reinforcement in aluminium metal matrix composites." In ADVANCES IN BASIC SCIENCE (ICABS 2019). AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5122398.

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Voyiadjis, George Z., and Rainer Echle. "Fatigue Damage in Metal Matrix Composites." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0488.

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Abstract In recent years the design and performance of aerospace vehicles changed due to enhancement and improvement in the design and the materials employed. Special consideration has to be given to the performance of the materials chosen for such vehicles. Titanium matrix composites (TMC) have been identified among the metal matrix composites as candidate materials capable of sustaining the arising loads while maintaining their structural integrity. Material behavior during fatigue loading has to be given special consideration since this loading condition is dominant during the flight regime. Material degradation due to fatigue loading is modeled using a micro-mechanical fatigue damage model for uni-directional metal matrix composites. The evolution of damage is considered at the constituent level by employing a damage criteria for each individual constituent. The overall material damage is obtained by using the Mori-Tanaka averaging scheme. A numerical implementation of the model is used to demonstrate its capabilities by presenting the analytical results for damage evolution in the fibers as well as in the matrix material for isothermal high cycle fatigue loading. Results for varying material and model parameters are also presented.
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Sundar, G., and N. Rajesh Jesudoss Hynes. "Corrosion issues in metal matrix composites & Bi-metals." In ADVANCES IN BASIC SCIENCE (ICABS 2019). AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5122399.

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Szostak, Marek, and Jacek Andrzejewski. "Thermal Properties of Polymer-Metal Composites." In ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/esda2014-20506.

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The objectives in this paper are to investigate the effects of the filler content and size on the effective thermal conductivity of the PE/Al; PE/Cu, PE/Fe and PE/bronze composites. The polymer matrix of the polymer/metal composites was two types of polyethylenes: LDPE and HDPE (from Basell Orlen). The following polymer/metal composites obtained by extrusion process containing: 10% by weight of Al, Cu, Fe and bronze powder in LDPE matrix and composites containing 5, 10, 15 and 20% by weight of Al flakes in HDPE polymer were prepared and tested. Adding in the extrusion process 10% by weight of bronze powder into the polyethylene, increased more than five times the thermal diffusivity of produced composite. Use as a filler 20% wt. of aluminum flake increases it by more than twice. The study showed the ability to produce polyethylene matrix composites with the addition of metal powder fillers (Al, Cu, Fe, and bronze). Analyzing the measuring results of thermal diffusivity coefficient by Angstrom method, it can be concluded that with the appropriate filler content, the particles are located close enough to each other to form a continuous conductive path, then the thermal diffusivity of the composite increases significantly.
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Reports on the topic "Metal matrix composites"

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Reynolds, G. H., and L. Yang. Plasma Joining of Metal Matrix Composites. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada176690.

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Reynolds, G. H., and L. Yang. Plasma Joining of Metal Matrix Composites. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada178731.

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Reynolds, G. H., and L. Yang. Plasma Joining of Metal Matrix Composites. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada181056.

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Reynolds, G. H., and L. Yang. Plasma Joining of Metal Matrix Composites. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada164095.

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Shelley, J. S., R. LeClaire, and J. Nichols. Metal Matrix Composites for Liquid Rocket Engines. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada410056.

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Newton, Crystal H. Implementation of the Military Handbook 17 for Polymer Matrix Composites and Metal Matrix Composites. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada278795.

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Newton, Crystal H. Implementation of the Military Handbook 17 for Polymer Matrix Composites and Metal Matrix Composites. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada285629.

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Newton, Crystal H. Implementation of the Military Handbook 17 for Polymer Matrix Composites and Metal Matrix Composites. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada285772.

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Viswanathan, S., W. Ren, W. D. Porter, C. R. Brinkman, A. S. Sabau, and R. M. Purgert. Metal Compression Forming of aluminum alloys and metal matrix composites. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/751621.

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Altshuler, Thomas L. Behavior of Metal Matrix Composites at Cryogenic Temperatures. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada213080.

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