Relevant bibliographies by topics / SiCp/Al composite

Academic literature on the topic 'SiCp/Al composite'

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Published: 10 December 2022
Last updated: 28 January 2023

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Journal articles on the topic "SiCp/Al composite"

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Chen, Yu Hong, Jian Jun Ma, Wen Jie Guo, Liang Jiang, and Peng Yuan Yang. "Microwave Sintering of SiCp/Al Composite." Key Engineering Materials 492 (September 2011): 138–41. http://dx.doi.org/10.4028/www.scientific.net/kem.492.138.

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Aluminum matrix composites reinforced by silicon carbide particles (SiCp/Al) were prepared using microwave sintering. The hardness, bending strength and compression strength of sintered composites had been measured. The results showed that SiCp/Al composite can be sintered by microwave in very short time. The oxidation or plating copper in silicon carbide surface can improve the mechanical properties of composites.
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Zhou, Xian Liang, Duo Sheng Li, Ai Hua Zou, Xiao Zhen Hua, G. Z. Ye, Qing Jun Chen, Jian Yun Zhang, and Yong Jin Tang. "Study on Atmospheric Corrosion Behaviour of Sicp/Al Composite." Advanced Materials Research 136 (October 2010): 275–78. http://dx.doi.org/10.4028/www.scientific.net/amr.136.275.

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SiCp/Al composite was fabricated by the method of pressureless-infiltration. In atmospheric environment, the atmospheric corrosion behavior of SiCp/Al composites (ZL101+49%SiC+5%Mg) was studied by mass loss, optical microscope (OM), scanning electron microscope (SEM), X-ray diffraction (XRD), energy dispersive spectrometer (EDS) and Fourier transform infrared spectroscopy (FTIR), respectivelhy.The results show that the corrosion rate of the SiCp/Al composites increases with increasing of time in atmospheric environment. Pitting corrosion is the main characteristic of SiCp/Al composite, and corrosion area gradually extends around with time increasing. At last, sheet like corrosion substrates distribute in the surface of n the SiCp/Al composites. Amorphous Al2O3 and amorphous AlxSO4yOHz are the main corrosion products.
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Li, Duo Sheng, X. L. Zhou, A. H. Zou, X. Z. Hua, G. Z. Ye, and Q. J. Chen. "Study on Micro-Deformation Behavior of Sicp/Al Composites at Low Stress." Advanced Materials Research 426 (January 2012): 147–50. http://dx.doi.org/10.4028/www.scientific.net/amr.426.147.

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In this paper, SiCp/Al composites were fabricated by spontaneous infiltration technology. The micro-deformation behavior (MDB) of low tress in some silicon carbide particulate reinforced aluminum composites (SiCp/Al composites) was investigated experimentally. The microstructure, micro-deformation of samples was analyzed by OM and WDW-50 respectively. The results show that, in aluminum matrix with incorporating SiCp, the distribution of SiCp was uniform. In the same other conditions, SiCp size of the composite plays an important role on MDB at low stress, and the micro-deformation performance of the SiCp/Al composite increases with decreasing of SiCp size. MDB of composites at low stress deeply depends on the matrix material, and MDB increases with increasing of the matrix strength. It was also found that, the micro-deformation of SiCp/Al composite was negative value in the early stages of low tensile stress, and the phenomenon can be explained by strain relaxation.
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Zhou, Xian Liang, Duo Sheng Li, Ai Hua Zou, Xiao Zhen Hua, Zhi Guo Ye, and Qing Jun Chen. "Thermal Expansion Behavior and Characteristic of SiCp/Al Composites." Advanced Materials Research 287-290 (July 2011): 658–61. http://dx.doi.org/10.4028/www.scientific.net/amr.287-290.658.

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SiCp/Al composites were fabricated by ceramic mold freedom infiltration and pressureless infiltration, respectively. The microstructure and phases are analyzed by metallurgical microscope and coefficient of thermal expansion of SiCp/Al composites were tested by thermal dilatometer. The results show that SiCp/Al composites are compact and uniform. SiC particles were dispersed uniformly in Al matrix, and SiCp segregation was not found in composites. Under a certain SiCp size range, space between SiCp decreases with decreasing of SiCp size, and CTE of SiCp/Al composites also decreases with decreasing of particles size. Compared with CTE of composite with pure aluminum as matrix, CTE of composite with ZL101 as matrix is less. Under the annealing process, CTE of SiCp/Al composites with ZL101 as matrix is less than that with the solution and aging, which indicated that its dimensional stability of resisting to temperature fluctuation is better, and thermal expansion behavior and characteristic of SiCp/Al composites are also better.
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Zhang, Zhen Lin, Zhi Feng Zhang, Jun Xu, and Wei Min Mao. "Rheological Behavior and Fluidity of Semi-Solid SiCp/A357 Composites with Different SiC Addition Levels." Solid State Phenomena 256 (September 2016): 126–32. http://dx.doi.org/10.4028/www.scientific.net/ssp.256.126.

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The apparent viscosities of the semi-solid SiCp/A357 composites with 0vol.%, 10vol.% and 20vol.% SiC particles manufactured by stir casting were investigated using a Couette type viscometer, and the composite fluidity was examined with a test casting. The results showed that, the viscosities of the semi-solid SiCp/A357 composites decreased with an increase in shear rate, but increased with the increasing of solid fraction, and apparent viscosity of 10vol.% SiCp/A357 composite was the lower than that of 20vol.% SiCp/A357 composite at the same solid fraction; and the composite fluidity results were in a good agreement with the viscosity ones.
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Wang, Bin, Shengguan Qu, and Xiaoqiang Li. "Preparation and Anodizing of SiCp/Al Composites with Relatively High Fraction of SiCp." Scanning 2018 (2018): 1–13. http://dx.doi.org/10.1155/2018/8945729.

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By properly proportioned SiC particles with different sizes and using squeeze infiltration process, SiCp/Al composites with high volume fraction of SiC content (Vp = 60.0%, 61.2%, 63.5%, 67.4%, and 68.0%) were achieved for optical application. The flexural strength of the prepared SiCp/Al composites was higher than 483 MPa and the elastic modulus was increased from 174.2 to 206.2 GPa. With an increase in SiC volume fraction, the flexural strength and Poisson’s ratio decreased with the increase in elastic modulus. After the anodic oxidation treatment, an oxidation film with porous structure was prepared on the surface of the composite and the oxidation film was uniformly distributed. The anodic oxide growth rate of composite decreased with SiC content increased and linearly increased with anodizing time.
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Li, Duo Sheng, Dun Wen Zuo, Xian Liang Zhou, Jian Yun Zhang, and Xiao Zhen Hua. "Wear-Resistant Property of SiCp/Al Composites." Key Engineering Materials 368-372 (February 2008): 1096–98. http://dx.doi.org/10.4028/www.scientific.net/kem.368-372.1096.

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Al alloy reinforced with SiCp (size: 70-220μm) was fabricated by pressureless-infiltration. Its wear resistant property was investigated under different heat-treatment conditions, and morphology of worn surface was examined. The results showed that the composite was integrated, uniform and compact, and its wear resistant property was better than that of the unreinforced matrix alloy. It was indicated that some rigid SiCp in the abraded surface of the composite could support part of loads and replace matrix to wear-tear, which improved the wear resistant property. Compared to annealing, solution aging strengthens Al alloy matrix and cohesion with SiCp, and the wear resistant property of composites was better. Combining interface is also an important factor which influences on wear resistant property. During the wear test, the smaller SiCp size, the more interfaces, there are more SiCp falling off because of loosening combining interface, which results in more wear-tearing value. The wear rate of composite increases with decreasing SiCp size, thus, the composite with larger SiCp has better wear-resistant property than that with smaller SiCp. At last, the wear mechanism of the composite was also studied, and it showed that abrasive wear dominated in the abrasion process.
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Chan, K. C., and J. Liang. "Effect of Microstructures on Deformation Behaviour of Aluminium Matrix Composites in Laser Bending." Textures and Microstructures 34, no. 1 (January 1, 2000): 43–54. http://dx.doi.org/10.1155/tsm.34.43.

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It is well known that the mechanical and deformation properties of metal matrix composites (MMCs) are related to their microstructures. However, less work has been carried out in laser bending to examine the dependency of microstructures of MMCs on deformation behaviour. In this paper, two aluminium-based metal matrix composites, Al2009/20 vol% SiCw and Al2009/20 vol% SiCp were investigated. A YAG laser was used to scan the composites both parallel and perpendicular to their rolling directions. It was reported that under the same processing conditions, a larger bending angle was obtained for the Al2009/SiCp composite. No significant change in microstructures was observed for both composites after bending. Experimental findings also revealed that for the particulate reinforced composite, a larger laser bending angle was obtained when the laser scanning direction was perpendicular to the rolling direction, whereas no significant difference was observed for the Al2009/SiCw composite. These phenomena were shown to relate to the shape and distribution of reinforcements.
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Li, Duo Sheng, Xian Liang Zhou, Ai Hua Zhou, Xiao Zhen Hua, and Y. W. Yu. "Study on Microstructure Characterization of SiCp/Al Composites." Advanced Materials Research 535-537 (June 2012): 227–30. http://dx.doi.org/10.4028/www.scientific.net/amr.535-537.227.

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ZL101 Al alloy reinforced with 55% silicon carbide particulate metal-matrix SiCp/Al composite has been fabricated by pressureless-infiltration. The microstructure characterization of composite has been studied by optical microscope (OM), scanning electron microscope (SEM), X-ray spectroscopy (EDX), respectively. The results show that the SiCp are uniformly distributed in Al alloy matrix, however, there are some casting defects such as shrinkage and gas porosities in the matrix. When Mg was added into the composite, it can improve wettability property of between Al matrixes and strengthen particle SiCp and decrease micro-defects such as gas porosities, the Microstructure of SiCp/Al composite prepared was compact and uniform. The SiCp particles evenly distributed in the matrix and without significant partial segregation phenomenon. It improves the whole performance of the composites.
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Liaw, P. K., R. Pitchumani, D. K. Hsu, H. Jeong, and S. C. Yao. "Nondestructive Eddy Current Evaluation of Anisotropic Conductivities of Silicon Carbide Reinforced Aluminum Metal-Matrix Composite Extrusions." Journal of Engineering for Gas Turbines and Power 116, no. 3 (July 1, 1994): 647–56. http://dx.doi.org/10.1115/1.2906869.

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Nondestructive eddy current methods were used to evaluate the electrical conductivity behavior of silicon-carbide particulate (SiCp) reinforced aluminum (Al) metal-matrix composite extrusions. The composites investigated included 2124, 6061, and 7091 Al base alloys reinforced by SiCp. The composite extrusions exhibited anisotropic conductivities with the maximum conductivity occurring along the extrusion plane. Microstructural characterization showed that the observed anisotropic conductivities could result from the preferred orientation distribution of SiCp. A theoretical model was formulated to quantify the influence of composite constituents (SiCp, intermetallics, and Al base alloy) on the anisotropic conductivities of the composites. The theoretical predictions of conductivities were found to be in good agreement with the experimental results.
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Dissertations / Theses on the topic "SiCp/Al composite"

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Bourgeois, Nadine. "Caractérisation et modélisation micromécanique du comportement et de l'endommagement d'un composte à matrice métallique Al/SiCp." Châtenay-Malabry, Ecole centrale de Paris, 1994. http://www.theses.fr/1994ECAP0353.

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Cette étude concerne le comportement en traction d'un composite aluminium renforce par 15% de particules de carbure de silicium, fabrique par pulvérisation-dépôt, extrudé, puis traité t6 ou t4. La géométrie et la répartition des renforts ont été mesurées par analyse d'images. Des essais de traction monotones ou avec charges et décharges ont permis une caractérisation globale du comportement et aussi une mesure de l'évolution de l'endommagement a travers celle du module d'Young. Les mécanismes d'endommagement ont été identifies lors d'essais dans l'enceinte d'un M. E. B. L'endommagement correspond à des ruptures de renforts. Suivant l'état métallurgique, l'amorçage se produit pour des déformations macroscopiques plus ou moins importantes. La modélisation du comportement de ce composite par une technique d'homogénéisation constitue la deuxième partie de ce travail. Le modèle utilisé, inspiré de la théorie d'Eshelby, est celui de Mori et Tanaka. L’extension de ce modèle au comportement élastoplastique utilise le concept de modules sécants et de contrainte équivalente de Von Mises. L’amorçage et l'évolution de l'endommagement sont décrits par l'introduction d'un critère statistique de rupture des particules, suivant une loi de Weibull. Les paramètres de Weibull ont été calés sur des mesures de fraction volumique et de taille des particules cassées. Des calculs par éléments finis ont permis de justifier le choix du comportement du renfort endommage équivalent qui remplace le renfort rompu. Le modèle a permis finalement de calculer le comportement du composite en traction pour les deux traitements thermiques. Les valeurs des paramètres introduits dans le modèle sont choisies en fonction des résultats expérimentaux. Courbes de traction, quantités et tailles de particules cassées, évolutions du module d'Young, prédites et mesurées sont très peu différentes
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Fouret, Charles. "Comportement et endommagement sous sollicitations monotones et cycliques d'un composite Al/SiCp de fonderie." Lille 1, 2000. http://www.theses.fr/2000LIL10192.

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Le but de cette etude est d'observer les mecanismes d'endommagement rencontres dans un composite a matrice metallique (cmm) al/sic p de fonderie, sous sollicitations monotones et cycliques, et de modeliser son comportement. Une etude bibliographique a realise une synthese des principaux travaux publies ces dernieres annees sur les cmm. Une etude experimentale a ete menee sur un cmm de fonderie, de matrice d'alliage d'aluminium, renforcee de 10% en volume de particules sic. Cette etude, realisee in-situ dans un microscope electronique a balayage, a mis en evidence les mecanismes d'endommagement du cmm, en traction monotone et sous sollicitations cycliques de traction-compression. Les essais monotones ont montre que l'endommagement en surface se manifestait par rupture de precipites, et par des decohesions entre precipites, particules et dendrites. Sous sollicitations cycliques, les mecanismes de propagation de fissure ont pu etre observes dans le domaine de la fatigue oligocyclique. Deux etapes ont pu etre distinguees. A faible niveau de contrainte en pointe de fissure, la propagation s'effectue dans l'eutectique, sans rupture de particules. A haut niveau de contrainte, la fissure peut egalement se propager par rupture de particules ou de dendrites. Le comportement mecanique du cmm a ete modelise par elements finis, sur un volume elementaire representatif (ver) compose de deux phases, matrice et particules ; la matrice est supposee avoir le meme comportement que l'alliage non renforce. Sous sollicitations tant monotones que cycliques, l'etude numerique a montre que le comportement mecanique du cmm ne pouvait pas etre modelise correctement par l'utilisation de ce ver.
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Qian, Daishu. "Microstructure and corrosion performance of excimer laser-melted AA2124-T4 aluminium alloy and SiCp/AA2124-T4 composite." Thesis, University of Manchester, 2016. https://www.research.manchester.ac.uk/portal/en/theses/microstructure-and-corrosion-performance-of-excimer-lasermelted-aa2124t4-aluminium-alloy-and-sicpaa2124t4-composite(705f8af9-2a7c-4188-91e4-fcf33d8f76f0).html.

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The present work studies the microstructure and corrosion behaviour of 25 vol.% SiCp/AA2124-T4 metal matrix composites (MMCs) and AA2124-T4 aluminium alloy; and also the capability of excimer laser surface melting (LSM) to improve the corrosion resistance of the SiCp/AA2124 MMC and the monolithic alloy (MA). Microstructural characterization has shown significant influence of the presence and size of SiC particles on the fine Al2Cu precipitate and Mg segregation at SiC/Al interfacial regions. Such precipitates are revealed to be active sites for corrosion initiation in the MMCs, while the preferential sites for corrosion initiation in the MA are the coarse intermetallics. Corrosion evaluation performed in a 0.6 M NaCl solution suggests that the corrosion resistance of the MMC reinforced with micrometre-sized SiC particles is inferior to that of the MA and the MMC reinforced with submicrometre-sized SiC particles. The submicrometre-sized SiC particles have little adverse effect on the corrosion resistance of the MMC due to the reduced interfacial precipitates. Thin films of up to several micrometres have been achieved by excimer LSM on both the MMC and the MA. The surface roughness and the thickness of the melted layer increase with increasing laser fluence. High number of pulses (40 P) results in significant porosity in the MA and networks of cracking in the MMC. A homogeneous layer without chemical segregation except the Cu-rich segregation bands has been obtained on the MA; while complex microstructures are observed for the MMC, including the Cu-rich segregation bands, Al-Si eutectic structure and microsegregation-free structure laid in sequence from the bottom of the melted layer to the top surface. The modelling work suggest that the presence of SiC particles gives rise in high temperatures in the melt pool, which is useful to explain the materials responses upon laser irradiation, such as decomposition of SiC, evaporation of matrix alloy, and oxides formation. The fast cooling rate up to 1011 K/s is responsible for the formation of microsegregation-free structure. Corrosion evaluation has indicated improvement of corrosion resistance of the MMC and the MA after excimer LSM due to the reduction of the intermetallics. For the laser-melted MA, the corrosion behaviour is governed by the surface morphology and the porosity. The significant rippled structure obtained under high laser fluence could lead to crevice corrosion in the valley between the ripples whilst the pores could provide penetrating routes for the chloride solution to reach the Cu-rich segregation bands, leading to the delamination of the melted layer. For the laser-melted MMC, corrosion mainly initiated at the SiC remnants, which are rich in Si. The corrosion sites of the laser-melted MMC are in the form of small cracked blisters.
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Quiles, Frank N. "An investigation of the effects of secondary processing on the fracture properties of a SiCp-6XXX Al composite." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA317262.

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Thesis (M.S. in Mechanical Engineering) Naval Postgraduate School, June 1996.
Thesis advisor(s): Indranath Dutta, Joe Wells. "June 1996." Includes bibliographical references. Also available online.
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Avenger, Donald Vincent. "Microstructure and aging response of SiCp reinforced A356 Al metal matrix composite subject to post fabrication thermomechanical processing." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1994. http://handle.dtic.mil/100.2/ADA292975.

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Dafir, Driss. "Etude de l'influence du renfort sur la cinétique de précipitation dans un composite 6061/SiCp élabore par métallurgie des poudres." Lyon, INSA, 1993. http://www.theses.fr/1993ISAL0049.

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Le but de ce travail a été une étude comparative des phénomènes de précipitation dans un alliage 6061 élaboré par métallurgie des poudres et dans le même alliage renforcé par une fraction volumique de 10% ou 20% de particules de SiC. Les cinétiques de précipitation ont été suivies essentiellement par mesure de pouvoir thermoélectrique. L'effet essentiel du renfort est d'abaisser le domaine de stabilité des phases semi-cohérente et incohérente et d'accélérer les cinétiques de précipitation. L'influence des diverses modifications microstructurales, dues au renfort, sur les cinétiques de précipitation a été analysée. En plus du rôle déjà bien connu des dislocations, ce travail met en évidence le rôle particulier ·des interfaces
The aim of this work was the investigation of the precipitation phenomena in a 6061 alloy elaborated by powder metallurgy either unreinforced or reinforced with a 10% or 20% volume fraction of SiC particles. The precipitation kinetics were mainly followed by TEP measurements and the TTP diagram of these materials was determined in the following range of temperature : from room temperature to 400 °C. The major effect of the reinforcement is to lower the stability domain of semi-coherent and coherent phases and to accelerate the precipitation kinetics. The influence of the microstructural modifications due to the introduction of the reinforcement on the precipitation kinetics were analysed. In addition ta the well-known effect of the dislocations, this work clearly evidences the particular role of the interfaces
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Lemnifi, Ahmed. "Influence of excimer laser surface melting on microstructure and corrosion behaviour of AA6061-T6 alloy and SiCp/AA6061-T6 composite." Thesis, University of Manchester, 2017. https://www.research.manchester.ac.uk/portal/en/theses/influence-of-excimer-laser-surface-melting-on-microstructure-and-corrosion-behaviour-of-aa6061t6-alloy-and-sicpaa6061t6-composite(5b945607-0479-411b-bb08-61e3c96a606e).html.

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This thesis presents an investigation of excimer laser surface melting (LSM) on AA6061-T6 alloy and SiCp/AA6061-T6 composite in terms of microstructure and corrosion behaviour. Hardness and wear resistance of the melted layer for both materials were also evaluated and compared with the untreated specimen to understand if the improvement of the corrosion resistance could be achieved without sacrificing the wear resistance. The intermetallic particles within the aluminium matrix are believed to initiate of both galvanic and pitting corrosion for both materials. To effectively dissolve these intermetallic particles, laser fluence from 1 to 8.5 J/cm2 with a number of pulses from 10, 25 to 50 were selected to achieve an optimisation of the LSM condition. It was found that the increase of laser fluence increased the melt depth, but also promoted the formation of defects such as micro-cracks and pores. For AA6061-T6 alloy, under the best laser condition (3 J/cm2 with 50 pulses), the amount of large intermetallic particles (2-10 µm), such as AlFeSi, AlFeMnSi and Mg2Si, were significantly reduced resulting in the formation of a relatively homogeneous and defect-free melt layer with only some small randomly distributed of intermetallic precipitates. For the SiCp/AA6061-T6 composite, under the best laser condition (6 J/cm2 with 25 pulses), decomposition of SiC particles was achieved as well as the dissolution of large AlMgSiCr and AlFeSi intermetallic particles in the melt layer. The melt layer had a relatively complex microstructure consisting of three different regions. MgO was found at the bottom of the melted layer which was discontinuous along the interface between the melted region and bulk material or in some places, at the bottom of the melted layer. The corrosion behaviour of both materials before and after LSM was evaluated using electrochemical measurements and immersion test in deaerated 0.6 M NaCl solution. After LSM the AA6061-T6 with and without SiC showed a better corrosion resistance compared with untreated alloys. The pitting potential of the LSM for both materials was shifted to a more positive value with a significant reduction of the passivation current density. In addition, an intergranular corrosion test based on the standard ASTM G110-92 showed that the LSM had significantly improved the corrosion resistance of both materials due to dissolution of intermetallic particles as well as the removal of the SiC particles in the composite material within the melted regions. In addition, the wear resistance of as-received SiCp/AA6061-T6 composites was found to be much higher than that of the LSM specimen. This is attributed to the decomposition of the majority of the SiCp in the melted region since the contribution to the hardness from the SiC particle in the untreated specimen is much greater that the Si-rich region in the melt layer after LSM.
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Yilmaz, Hamdi Sencer. "Characterization Of Silicon Carbide Particulate Reinforced Squeeze Cast Aluminum 7075 Matrix Composite." Master's thesis, METU, 2004. http://etd.lib.metu.edu.tr/upload/3/12605261/index.pdf.

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The aim of this study is to investigate the mechanical behavior and its relation with processing and microstructure of the silicon carbide particulate (SiCp) reinforced aluminum matrix composite. Aluminum 7075 alloy is chosen as matrix alloy, in which zinc is the main alloying element. Four different additions of SiCp were used and the weight fractions were 10%, 15%, 20% and 30%. Composites were processed by with squeeze casting and the applied pressure during casting was 80 MPa. The mould is specially designed to produce both specimens ready for tensile and three point bending tests. Both as-cast and heat treated aluminum composites were examined and T6 heat treatment was applied. Three point bending tests were performed to reveal the fracture strength of aluminum composites. 10wt% SiCp aluminum composites showed the maximum flexural strength in both as-cast and heat treated composites. The mechanical test results revealed that precipitated phases in heat treated composites, behaved like fine silicon carbide particulates and they acted as barriers to dislocation motion. Maximum flexural strength increased about 40 MPa (10%) in as-cast and 180 MPa (44%) in heat treated composites. Tensile testing was also conducted to verify the results of the three point bending tests. Hardness tests were done to find the effect of silicon carbide addition and to find the peak hardness in heat treatment. For as-cast specimens hardness values increased from 133 to 188 Vickers hardness (10 kg.) with increase in SiCp content from 0 to 30wt% and for heat treatment specimens hardness values increased from 171 to 221 Vickers hardness (10 kg.). The peak hardness values were obtained at 24 hours precipitation heat treatment. SEM studies were carried out to examine the heat treated composites, to take SEM photographs and to obtain a general elemental analysis. Theoretical volume percentage addition of SiCp was checked with Clemex Image Analyzer program. Distribution of SiCp was determined by mettalographic examination. Second phases that were formed during heat treatment was searched by x-ray analysis.
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Gomes, Márcia Aparecida. "Caracterização mecânica e microestrutural de compósitos de matriz metálica Al/SiCp e Al/Al2O3p obtidos via interação por laminação acumulativa." Universidade de São Paulo, 2015. http://www.teses.usp.br/teses/disponiveis/18/18158/tde-01032016-131333/.

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Compósitos de matriz metálica (CMM) reforçados com dois tipos de particulado cerâmico foram produzidos por meio do processo ARB (Accumulative Roll Bonding) a fim de estudar os efeitos destes no que diz respeito às propriedades mecânicas e microestruturais. ARB é um processo de deformação plástica severa aplicada originalmente a uma pilha de lâminas metálicas, a qual é laminada, seccionada em duas metades, as quais são empilhadas e novamente laminadas, e assim por diante, desenvolvido com o propósito de reduzir o tamanho de grão e aumentar a resistência mecânica do produto final. O processo é econômico e capaz de produzir de folhas ultrafinas a placas espessas, sem que haja restrição de quantidade. Confeccionou-se CMM de alumínio reforçados com partículas de carbeto de silício (Al+SiCp) e alumina (e Al+Al2O3p) com granulometria média de 40µm, as quais foram caracterizadas microestruturalmente e ensaiadas em tração até a falha, cuja análise foi conduzida via microscopia eletrônica de varredura. Ambas as amostras obtiveram ganho em sua resistência mecânica, comparadas ao alumínio monolítico (sem adição de partículas de reforço) e alumínio recozido. Foram ensaiados em tração corpos de prova com e sem presença de entalhe, sendo que as peças entalhadas apresentaram comportamento esperado de aumento de resistência mecânica e baixo alongamento e fratura de aspecto frágil. De acordo com análise feita por fratografia houve boa ancoragem e dispersão das partículas de reforço na matriz.
Metal matrix composite (CMM) reinforced with two types of ceramic particles have been produced through the process ARB (Accumulative Roll Bonding) in order to study their effect as regards the mechanical and microstructural properties. ARB is a severe plastic deformation process originally applied to a stack of metal sheets, which is laminated, sectioned into two halves, which are stacked and rolled again, and so on, developed with the purpose of reducing the grain size and increase the mechanical strength of the final product. The process is economical and capable of producing ultrafine sheets to thicker plates without much restriction. Were fabricated CMM of the aluminum reinforced with particles of silicon carbide (Al + SiCp) and alumina (and Al + Al2O3p) with an average particle size of 40μm, which are characterized microstructurally and tested in tension until failure, whose analysis was conducted via scanning electron microscopy. Both samples were successful in its mechanical strength compared to the monolithic aluminum (without addition of reinforcing particles) and annealed aluminum. They were tested for tensile specimens with and without the presence of notch, and the carved pieces showed strength-enhancing behavior and low elongation and frail fracture. According to analysis by fractography was good anchoring and reinforcement particles dispersed in the matrix.
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Li, Xianyao. "Wear behaviour and microstructural characterization of worn surfaces and wear debris of a high purity Al and an Al-Si alloy and an Al-Si/SiCp composite sliding against an M2 steel." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape8/PQDD_0015/NQ45008.pdf.

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Books on the topic "SiCp/Al composite"

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Quiles, Frank N. An investigation of the effects of secondary processing on the fracture properties of a SiCp-6XXX Al composite. Monterey, Calif: Naval Postgraduate School, 1996.

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Castelli, Michael G. Thermomechanical testing techniques for high-temperature composites: TMF behavior of SiC(SCS-6)/Ti-15-3. [Washington, D.C.]: NASA, 1990.

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International Metallographic Society. Technical Meeting. The roll [sic] of characterization in understanding environmental degradation of materials: Proceedings of the thirtieth annual Technical Meeting of the International Metallographic Society. Columbus, Ohio: International Metallographic Society, 1998.

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DellaCorte, Christopher. Experimentally determined wear behavior of an Al2O3-SiC composite from 25 to 1200 ̊C. [Washington, D.C.]: NASA, 1990.

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DellaCorte, Christopher. Experimentally determined wear behavior of an Al2O3-SiC composite from 25 to 1200 ̊C. [Washington, D.C.]: NASA, 1990.

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Murthy, Pappu L. N. Characterizing the properties of a woven SiC/SiC composite using W-CEMCAN computer code. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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Akira, Kohyama, and CREST International Symposium on SiC/SiC Composite Materials Research and Development and its Application to Advanced Energy Systems (2002 : Kyoto, Japan)., eds. Advanced SiC/SiC ceramic composites: Developments and applications in energy systems. Westerville, Ohio: American Ceramic Society, 2002.

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Robinson, David N. Limit pressure of a circumferentially reinforced SiC/Ti ring. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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name, No. Advanced SiC/SiC ceramic composites: Developments and applications in energy systems. Westerville, OH: The American Ceramic Society, 2002.

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Hyer, M. W. Innovative design of composite structures: Design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA, 1994.

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Book chapters on the topic "SiCp/Al composite"

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Biner, S. B. "Fatigue Characteristics of SiCp-Metal Matrix Composite." In Mechanical Behavior of Materials, 101–7. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-1968-6_11.

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Geng, Lin, and Yi Wu Yan. "Effects of Particle Size on the Thermal Physical Properties of SiCp/Al Composites." In Composite Materials V, 131–34. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-451-0.131.

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Singh, Raj Kumar, Sanjay Soni, and Pushyamitra Mishra. "Low-Stress Abrasion Response of Heat-Treated LM25–SiCp Composite." In Artificial Intelligence, Internet of Things (IoT) and Smart Materials for Energy Applications, 255–68. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781003220176-16.

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Patel, Satyendra Kumar, Ashwani Pratap, Priyabrata Sahoo, Binayaka Nahak, and Tej Pratap. "Cutting Force Analysis in Micro-milling of Al6061-SiCp Composite." In Springer Proceedings in Materials, 285–95. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-0182-8_22.

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Liaw, P. K., R. Pitchumani, S. C. Yao, D. K. Hsu, B. Foster, and H. Jeong. "Modeling Anisotropic Conductivity Behavior of SiCp/Al Metal- Matrix Composite Extrusions." In Review of Progress in Quantitative Nondestructive Evaluation, 1329–36. Boston, MA: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-2848-7_170.

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Bochenek, A., and K. N. Braszczyñska. "Relations between the Structure and Mechanical Properties of the MgAl-SiCp Composite." In Microstructural Investigation and Analysis, 233–36. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527606165.ch36.

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Zheng, Hansen, Zhifeng Zhang, and Yuelong Bai. "Simulation and Experimental Study on Hot Forging Process of SiCp/2A14 Composite." In Springer Proceedings in Physics, 41–49. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-5944-6_5.

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Kumar, J. Prem, V. R. Rajeev, K. Krishnakumar, and M. Hashim. "Microstructure and Hardness Evaluation of Functionally Graded A356-20 wt.% SiCP Composite." In Lecture Notes in Mechanical Engineering, 235–43. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-8025-3_23.

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Zhang, Q., Zi Yang Xiu, Mei Hui Song, and Gao Hui Wu. "Microstructure and Properties of a 70vol.% SiCp/Al-12Si Composite for Electronic Packaging." In Materials Science Forum, 881–84. Stafa: Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-960-1.881.

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Zhang, Qiang, Jie Cai Han, Ye Zhu, and Gao Hui Wu. "Microstructure and Hardness Performance of a SiCp/Al Composite by Pressureless Infiltration Technique." In Key Engineering Materials, 1318–21. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-456-1.1318.

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Conference papers on the topic "SiCp/Al composite"

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Hu, M., S. Kang, and K. Euh. "Microstructures of Sprayed SiCp/Al Composites." In ITSC2005, edited by E. Lugscheider. Verlag für Schweißen und verwandte Verfahren DVS-Verlag GmbH, 2005. http://dx.doi.org/10.31399/asm.cp.itsc2005p0590.

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Abstract The SiCp/Al composite was fabricated by a plasma spraying technique. By mean of OM SEM, TEM, XRD, SAED, EDS techniques, the microstructures for sprayed SiCp/Al composite were investigated in detail. The composite consisted of SiC and Al, along with single crystal Si and amorphorous Si, and tiny Al2O3. On the whole, the interfaces between SiC particle and Al bonded well, and tiny reactants like Al2O3 can be found near the interfaces. The mechanisms of chemical reactions were given during spraying. The nano-Al grains and nano-Al particles were seen in the sprayed composite. The formation mechanism of nano-Al grains and particles of SiCp/ Al composite was explained. Some interface relationships existed in the sprayed composite.
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Liaw, P. K., R. Pitchumani, S. C. Yao, D. K. Hsu, and H. Jeong. "Nondestructive Eddy Current Evaluation of Anisotropic Conductivities of Silicon Carbide Reinforced Aluminum Metal-Matrix Composite Extrusions." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-015.

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Nondestructive eddy current methods were used to evaluate the electrical conductivity behavior of silicon-carbide particulate (SiCp) reinforced aluminum (Al) metal-matrix composite extrusions. The composites investigated included 2124, 6061 and 7091 Al base alloys reinforced by SiCp. The composite extrusions exhibited anisotropic conductivities with the maximum conductivity occurring along the extrusion plane. Microstructural characterization showed that the observed anisotropic conductivities could result from the preferred orientation distribution of SiCp. A theoretical model was formulated to quantify the influence of composite constituents (SiCp, intermetallics and Al base alloy) on the anisotropic conductivities of the composites. The theoretical predictions of conductivities were found to be in good agreement with the experimental results.
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Kang, Guozheng. "Uniaxial Ratchetting of SiCP/6061Al Alloy Composites at Room and High Temperatures." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-79361.

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The uniaxial strain cyclic characteristics and ratcheting behaviors of T6-treated SiCP/6061Al alloy composites were studied experimentally at room and high temperatures (573K). The cyclic softening/hardening and ratcheting behaviors of T6-treated composites and un-reinforced matrix were investigated in different loading conditions and with two volume fractions of SiC particulates. It is shown that the cyclic softening/ hardening and ratcheting behaviors of the composites are similar to those of the un-reinforced matrix in macro-scale, i.e., the ratcheting also occurs in the composites during the cyclic stressing with non-zero mean stress, and the ratcheting strain increases with the increasing of stress amplitude and mean stress; however, the addition of SiC particulates into the matrix increases the resistance of the composite to the ratcheting, and the ratcheting strain decreases as the volume fraction of SiC particulates increases. It can be also concluded that the cyclic deformation of the composites has a great temperature-dependence. Some significant conclusions are obtained, which are useful to construct a constitutive model to describe the cyclic deformation of the composites.
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Skolnik, D. A., H. T. Liu, L. Z. Sun, and H. C. Wu. "Anisotropic Elastoplastic Behavior of SiCp/Al Composite Sheets." In ASME 2004 International Mechanical Engineering Congress and Exposition. ASMEDC, 2004. http://dx.doi.org/10.1115/imece2004-60635.

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Experimental research was performed to study the anisotropic elastoplastic responses of SiCp/Al composite sheets. To investigate the effects of the composite processing, two sets of specimens cut from the heat-treated and as-rolled composite sheets are tested using a universal material-testing machine. The dependence of the strength, plastic flow, and strain ratios on the rolling angles are discussed in detail. To model the phenomena observed in the experiments, a micromechanics based damage framework is developed. The interfacial debonding and the rolling angle’s effects are integrated into this model. Good consistence between the experimental results and the analytical predications shows the validity of the theoretical model.
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Karibeeran, Shanmuga Sundaram, Dhanalakshmi Sathishkumar, Sankar Ramaiyan, and Rajamanickam Subban. "Investigations on the Structure and Properties of the Hot Extruded AA2014-Nano SiCp Composite." In ASME 2018 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/imece2018-87237.

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Aluminium based metal matrix composites with nano particle reinforcement are currently finding wide spread applications in automobile, aerospace and space structures because of their high strength, fatigue life, excellent wear resistance, low thermal coefficient value. However, in order to use these materials for critical automotive applications, extensive study in terms of manufacturing feasibility of the composites have to be carried out. Based on the objectives, the present investigation focuses on the development of Aluminium-SiC nano composite for structural applications. The aim of this research work is to arrive at an optimum weight faction of nano particle which gives the highest properties of the nano composite. The composites were produced by stir casting route. The base alloy and the composites were extruded and subsequently subjected to age hardening treatment. Microstructural evaluation, hardness studies were carried out on both the base alloy and the composites in the as-cast and extruded conditions. The effect of extrusion on the microstructure and properties of the AA2014-0.8 wt.%SiC composites have been discussed in detail.
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Shu, Kuen Ming, Hung Rung Shih, Wen Feng Lin, and G. C. Tu. "Hybrid EDM and Grinding Hard Materials Using a Metal Matrix Composite Electrode." In ASME 7th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2004. http://dx.doi.org/10.1115/esda2004-58098.

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Electrical discharge machining (EDM) has been shown to be a versatile method for machining difficult-to-work materials including heated-treated steels, tungsten carbides and various conductive ceramics. However, low machining efficiency is one of the main EDM disadvantages. The topic of how to reduce machining time and maintains reasonable accuracy has always been of research interest. The main object of the present work was to develop an electrical discharge machining and grinding (EDMG) methodology to remove the re-solidified layer through the grinding induced by a metal matrix composite electrode prior to the re-solidified layer solidification. A metal matrix composite (Cu/SiCp) electrode, with an electroless pretreatment of Cu coating on SiCp to enhance bonding status between Cu and SiCp, with a rotating device was made and employed to study the EDMG technology. Machinabilities of mold material, HPM50 mold steel and P20 WC/Co, were investigated by the combined technologies of EDMG. The machined surfaces of these materials were examined by scanning electron microscopy (SEM) and their surface roughness measured by a profile meter. From the experimental results, it was found that higher material removal rate and lower surface roughness can be achieved when suitable electrode rotating speed, SiCp size and working current are chosen. In addition, the surface roughness of both materials could be improved as compared with that following the EDM process.
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Arhami, M., F. Sarioglu, and A. Kalkanli. "Effect of Heat-Treatment and Reinforcement With Silicon Carbide on the Microstructure and Mechanical Properties of AlFeVSi Alloy." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-42073.

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The aging response of Al-Fe-V-Si composite was compared with the un-reinforced alloy. The effects of solutionizing time, alloying element and SiC reinforcement on the age hardening response, microstructure and mechanical properties of these alloy and its composites was also investigated. The study was performed by T6 heat treatment at three different solutionizing times. Room temperature tensile testing was conducted for peak aged specimens to determine the effect of this heat treatment on the strength of squeezed cast un-reinforced and reinforced Al-Fe-V-Si alloy with SiC particles. The presence of SiC particles accelerated the aging kinetics of the composites compared to the unreinforced alloys. The time to reach peak age hardness was decreased by addition of SiCp. Mainly two different Fe-intermetallics; small α-Al7(Fe, V)3Si and large β-Al18Fe11Si phases were present in the system studied. The fracture surfaces of composites revealed decohesion of SiC particles from the matrix and cracking of needle like-β intermetallics was observed.
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Bains, Preetkanwal Singh, H. S. Payal, and Sarabjeet Singh Sidhu. "Analysis of Coefficient of Thermal Expansion and Thermal Conductivity of Bi-Modal SiC/A356 Composites Fabricated via Powder Metallurgy Route." In ASME 2017 Heat Transfer Summer Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/ht2017-5122.

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The present study investigates the thermal conductivity and coefficient of thermal expansion of bimodal SiCp reinforced Aluminum matrix composites formed via powder metallurgy method. The after-effects of proportion of particulate reinforcement as size distribution and sintering parameters on the thermal properties have been explored. The Box-Behnken design for response surface methodology was adopted to recognize the significance of chosen variables on the thermal conductivity and coefficient of thermal expansion of the composite. It is witnessed that the thermal conductivity and coefficient of thermal expansion enhanced due to increase in fine SiC particulates volume fraction. It has been exhibited that the fine SiC particulates (37μm) doped Al-matrix occupied interstitial positions and developed continuous SiC-matrix network. SEMs were conducted to evaluate the microstructure architecture for MMCs.
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Vaidya, Rajendra U., and Anna K. Zurek. "Dynamic mechanical deformation of a SiCp/Al-Li (8090) composite." In High-pressure science and technology—1993. AIP, 1994. http://dx.doi.org/10.1063/1.46213.

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Purohit, Rajesh, and Rakesh Sagar. "Finite-Element Analysis of Al-SiCp Composite Poppet Valve Guides." In International Mobility Engineering Congress & Exposition 2005 - SAE India Technology for Emerging Markets. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-26-310.

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Reports on the topic "SiCp/Al composite"

1

Youngblood, G. E., R. H. Jones, Akira Kohyama, Yutai Katoh, Akira Hasegawa, L. Snead, and R. Scholz. The HFIR 14J irradiation SiC/SiC composite and SiC fiber collaboration. Office of Scientific and Technical Information (OSTI), September 1998. http://dx.doi.org/10.2172/330620.

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Singh, Gyanender, Stephen T. Gonczy, Edgar Lara-Curzio, and Yutai Kato. Interlaboratory Round Robin Testing of SiC/SiC Composite Tubes. Office of Scientific and Technical Information (OSTI), August 2016. http://dx.doi.org/10.2172/1513437.

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Youngblood, G. E., and R. H. Jones. Methods of radiation effects evaluation of SiC/SiC composite and SiC fibers. Office of Scientific and Technical Information (OSTI), March 1998. http://dx.doi.org/10.2172/335383.

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Yueh, Ken. SiC Composite for Fuel Structure Applications. Office of Scientific and Technical Information (OSTI), December 2017. http://dx.doi.org/10.2172/1415452.

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

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Zinkle, S. J., and L. L. Snead. Thermophysical and mechanical properties of SiC/SiC composites. Office of Scientific and Technical Information (OSTI), September 1998. http://dx.doi.org/10.2172/330618.

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Stinton, D. P., E. R. Kupp, and J. W. Hurley. Oxidation-resistant interface coatings for SiC/SiC composites. Office of Scientific and Technical Information (OSTI), June 1996. http://dx.doi.org/10.2172/450753.

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Ghoniem, N. M. Radiation effects and micromechanics of SiC/SiC composites. Office of Scientific and Technical Information (OSTI), January 1991. http://dx.doi.org/10.2172/6181622.

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Ghoniem, N. M. Radiation effects and micromechanics of SiC/SiC composites. Office of Scientific and Technical Information (OSTI), January 1992. http://dx.doi.org/10.2172/6917051.

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Coon, D. Vitreous joining of SiC fiber reinforced SiC composites. Office of Scientific and Technical Information (OSTI), December 1989. http://dx.doi.org/10.2172/6973365.

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