Relevant bibliographies by topics / 5086 aluminium alloy

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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 '5086 aluminium alloy'

Author: Grafiati
Published: 4 June 2021
Last updated: 10 February 2022

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Journal articles on the topic "5086 aluminium alloy"

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Rajesh Kannan, Subburaj, J. Lakshmipathy, M. Vignesh Kumar, K. Manisekar, and N. Murugan. "Optimization Analysis of Process Parameters of Friction Stir Welded Dissimilar Joints of Aluminium Alloys." Applied Mechanics and Materials 867 (July 2017): 112–18. http://dx.doi.org/10.4028/www.scientific.net/amm.867.112.

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Friction stir welding (FSW) is one of the new technique for welding materials in solid state welding process. In this proposed work we are using FSW to join the two dissimilar alloys of aluminium. The 6mm thick aluminum plates of aluminium 5086 and aluminum 7075 plates are considered for welding. These have been considered due to their application in various fields. In this experimental process Taguchi’s L9 orthogonal array method is used for optimizing the three process parameters namely rotational speed, axial force and welding speed. To produce a better joint the tensile strength is predicted for the optimum welding parameters and also their percentage of contribution is calculated, by applying the effect of analysis of variance. Depends upon the experimental study, the rotational speed is found better over the other process parameters, which enhances the quality of the weld. The tensile strength has been found for the optimum parameters and the result found during the experiment was 290Mpa which was higher than the base metal strength of aluminium 5086 alloy. The SEM fractograph analysis was done on the optimum parameters welded joints to show the fracture behaviour of tensile test which justifies the visual inspection results of brittle and ductile failures.
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Narayanasamy, R., M. Ravi chandran, C. Sathiya Narayanan, N. L. Parthasarathi, and R. Ravindran. "Effect of annealing temperature on void coalescence in 5086 aluminium alloy formed under different stress conditions." International Journal of Mechanics and Materials in Design 3, no. 4 (June 13, 2007): 293–307. http://dx.doi.org/10.1007/s10999-007-9025-3.

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Narayanasamy, R., J. Satheesh, and C. Sathiya Narayanan. "Effect of annealing on combined forming, fracture and wrinkling limit diagram of Aluminium 5086 alloy sheets." International Journal of Mechanics and Materials in Design 4, no. 1 (December 4, 2007): 31–43. http://dx.doi.org/10.1007/s10999-007-9052-0.

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Zhu, Sheng, Guo Feng Han, Xiao Ming Wang, Yu Xiang Liu, and Zhi Qian Wang. "Electrochemical Characteristics of TiAl Coating on Aluminum Alloy Surface by Supersonic Particles Deposition." Advanced Materials Research 1051 (October 2014): 199–203. http://dx.doi.org/10.4028/www.scientific.net/amr.1051.199.

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In this study, Ti-45Al-7Nb-4V alloy protective coating which base on γ-TiAl phase was deposited on the surface of 5803 aluminum alloy by supersonic particles deposition technology. Researchers observed the micro-structure of the TiAl alloy casting and coating by SEM, and researched the electrochemical characteristics and the galvanic corrosion between TA2 titanium alloy and 5083 aluminum alloy or TiAl alloy casting and coating by electrochemical work station. The results show that,the galvanic corrosion current between 5083 aluminium alloy and TA2 titanium alloy declines from 16.2μA to 0.27μA after TiAl protecting coatings are prepared on the substrates, besides, the corrosion susceptibility drops from E degree to A degree. It also manifests that the 5083 aluminium alloy with Ti-45Al-7Nb-4V coatings can be contacted and utilized with TA2 titanium alloy directly, which tackles the issues of gavanic corrosion prevention between aluminium alloys and titanium alloys.
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Wongpreedee, Kageeporn, Panphot Ruethaitananon, and Tawinun Isariyamateekun. "Interface Layers of Ag-Al Fusing Metals by Casting Processes." Advanced Materials Research 787 (September 2013): 341–45. http://dx.doi.org/10.4028/www.scientific.net/amr.787.341.

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The materials of fusing metals commercially used in the jewelry niche marketing is seen as precious metals. An innovation of fusing metals searched for new materials to differentiate from the markets for mass production. In this research, it studied the bonding processes of silver and aluminium metals by casting processes for mass productions. The studies had been varied parameters on the types of aluminium and process temperature controls. This research had used two types of aluminium which were pure aluminium 99.99% and aluminum 5083 alloys bonding with pure silver 99.99%. The temperatures had been specified for two factors including casting temperature at X1, X2 and flasking temperature at Y1, Y2. From the results, it was found that the casting temperature at 730°C and the flasking temperature at 230 °C of pure silver-aluminum 5083 alloys bonding had the thinnest average thickness of interface at 427.29 μm. The microstructure of pure silver-aluminum 5083 alloy bonding was revealed eutectic-like structures at the interfaces. The EDS analysis showed the results of compounds at interface layers of Ag sides giving Ag2Al intermetallics on pure silver-aluminum 5083 alloy bonding unlike pure silver-pure aluminium bonding giving Ag3Al intermetallics.
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Ilangovan, M., S. Rajendra Boopathy, and V. Balasubramanian. "Effect of tool pin profile on microstructure and tensile properties of friction stir welded dissimilar AA 6061–AA 5086 aluminium alloy joints." Defence Technology 11, no. 2 (June 2015): 174–84. http://dx.doi.org/10.1016/j.dt.2015.01.004.

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Shibayanagi, Toshiya, and Masaaki Naka. "Control of Grain Size and Texture in Al Alloys Utilizing Friction Stir Processing." Materials Science Forum 539-543 (March 2007): 3769–74. http://dx.doi.org/10.4028/www.scientific.net/msf.539-543.3769.

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The present paper deals with the control of microstructure of friction stir processed aluminum alloys focusing on grain refinement, thermal stability at elevated temperature and texture development in some aluminum alloys such as 5083, 6061 and 7075 commercial aluminum alloys. 3mm thickness plates of 5083, 6061 and 7075 Al alloys were friction stir processed/welded with several rotation speeds and travelling speeds. Optical microscopy revealed the grain refinement in the stirred zone of each alloy and the average grain size decreased with decreasing rotation speed under various travelling speeds. Annealing of the joints brought about abnormal grain growth at temperatures higher than 773K for 5083 alloy. Critical temperature of the abnormal grain growth tended to decrease as the rotation speed decreased for the fixed travelling speed. Dissimilar joining of 5083 Al alloy to 6061 Al alloy also showed abnormal grain growth when annealed at 773K. A peculiar texture development of 7075 Al joint showing (111)//ND-oriented grains existing throughout the nugget was revealed by EBSP analysis.
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Dudzik, Krzysztof, and Mirosław Czechowski. "Influence of Joining Method for Mechanical Properties of 5083, 5059 and 7020 Aluminum Alloys Joints." Solid State Phenomena 220-221 (January 2015): 583–88. http://dx.doi.org/10.4028/www.scientific.net/ssp.220-221.583.

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The paper presents the research results on the mechanical properties of aluminum alloy 7020 and its FSW and MIG welded joints. For comparison, alloy 5083 – the most currently used in shipbuilding alloy was chosen as well as 5059 – the new high-strength alloy. Besides, the native material alloys there were investigated their joints welded by FSW and MIG – the same methods as alloy 7020. Welding parameters used for the connection of the sheets made of 7020, 5083 and 5059 alloys were presented. Metallographic analysis showed the correct construction of structural bonded joints.Friction Stir Welding (FSW) – a new technology can be successfully used for butt welding of different types of aluminum alloy sheets. FSW method can be an alternative to traditional arc welding methods, especially MIG, which is the most common method of joining aluminum alloys used in shipbuilding. The research was carried out using a static tensile test in accordance with the requirements of the Polish Standards PN-EN ISO 4136:2011 and PN-EN ISO 6892-1:2010. Flat samples cut perpendicular to the direction of rolling were used. The research was conducted at the temperature of +20 oC.Friction stir welded joints of tested alloys have higher strength properties as compared to MIG welded joints. The 7020 alloy has higher strength properties then alloys 5083 and 5059. The yield stress is higher by 14.8% as compared to alloy 5083, and by 11.7% as compared to the alloy 5059. Plastic properties of alloy 7020 are the lowest, but with reserves meet the requirements of classification societies. The joints welded by FSW of alloy 7020 have the highest strength properties of all researched joints – higher then alloys 5083 and 5059 joints welded by FSW and joints of all alloys welded by MIG.
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Nhan, Phan Thanh, Tran Minh Khang, and Tran Hung Tra. "Investigation of AA5083 T-lap joint fabricated by friction stir welding." Vietnam Journal of Science and Technology 57, no. 4 (July 1, 2019): 457. http://dx.doi.org/10.15625/2525-2518/57/4/13535.

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Transportation industries are faced to big maters that the scientists focus on, such as energy saving and ecologically sustainable products. Therefore, many innovative solutions are delivered that will support environmental preservation but meet industries’ requirements for greater productivity and minimized operational costs. Aluminium alloys have successfully contributed to meeting the rising demand for lightweight structures. Recently, notable developments in aluminium welding techniques have resolved many welding related problems, although some problems need to be addressed. In this paper, 5083 aluminium alloy T-lap-joints were successfully fabricated by friction stir welding with various welding regimes. The defects morphology in the T-joints was experimentally observed and analyzed by a high magnification microscope. The roles of the grain microstructure and the effects of defects morphology in the mechanical behavior of the T-joint was investigated. In addition, the fracture locations and the fracture surface of the failure specimens were observed and discussed as well. Results indicate that the fracture of T-joints along the stringer is attributed to the bonding line defects, kissing bond defects and the tunnel defects. The result also shows, in the T-joints of 5083 aluminum alloy, the welding parameters influence significantly on the features and sizes of the defects.
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Wu, Jian Xin, Chong Gao, Rui Yin Huang, Zhen Shan Liu, and Pi Zhi Zhao. "Effect of Cold Deformation and Annealing on Microstructure and Mechanical Properties of 5083 Aluminum Alloy Sheets." Materials Science Forum 913 (February 2018): 49–54. http://dx.doi.org/10.4028/www.scientific.net/msf.913.49.

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5083 aluminum alloy, due to moderate strength, good thermal conductivity and formability, is an ideal structural material for car production. Influence of cold rolling process on microstructures and mechanical properties of 5083 aluminum alloys is significant and research hotspots. In this paper, cold deformation and annealing processes on grains, tensile properties and anisotropies of 5083 alloy sheets were studied. Results showed that incomplete recrystallization occured on 5083 alloy sheets when annealing temperature was at 300°C. The degree of recrystallization increased slightly with the cold deformation raised from 30% to 50% and varied slightly with prolonged annealing time from 2h to 4h. Furthermore, fully recrystallization occurred on 5083 alloy sheets at the annealing temperature above 320°C. Tensile strength of 5083 alloy sheets reduced significantly when the annealing temperature was raised from 300°C to 320°C, while it varied slightly when the annealing temperature continued to rise to 380°C.
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Dissertations / Theses on the topic "5086 aluminium alloy"

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Batigun, Caner. "Determination Of Welding Parameter Dependent Hot Cracking Susceptibility Of 5086-h32 Aluminium Alloy With The Use Of Mvt Method." Phd thesis, METU, 2005. http://etd.lib.metu.edu.tr/upload/3/12605721/index.pdf.

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Hot cracking is a serious problem that encounters during welding of aluminium-magnesium alloys. In the present study, solidification and liquation type of hot cracks in weld metal and the heat-affected zones of 5086-H32 aluminium alloy were investigated by using Modified Varestraint Test (MVT) with TIG-AC and TIG-DC welding. With determining the size, type and number of cracks, a relation was established between welding line energy and strain on the hot crack formation. This information was used to determine the hot crack safe parameter ranges. The hot cracking tendency as a function of applied parameters were discussed in the frame of temperature fields around the moving heat source. Moreover, the characteristic hot crack locations on the 5086-H32 MVT specimens were generalized. The results of the study indicated that the increase in line energy and strain increased the hot cracking tendency of the specified aluminium alloy. In the low line energy range, the main hot cracking mechanism is the solidification cracking which could be overcome by the use of a suitable filler material. At high line energy range, due to the increased amount of interdendritic liquid, the amount of solidification cracking decreases by healing mechanism. However, because of the enlarged-temperature-field around the weld zone, fraction of HAZ cracking increases. The comparison between the hot cracking tendencies in low and high line energies indicates that the low line energy ranges with low augmented strains resulted in hot crack safer parameters.
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Chu, XingRong. "Caractérisation expérimentale et prédiction de la formabilité d'un alliage d'aluminium en fonction de la température et de la vitesse de déformation." Phd thesis, INSA de Rennes, 2013. http://tel.archives-ouvertes.fr/tel-00910093.

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Les procédés de mise en forme de tôles minces sont très largement répandus dans l'industrie. Néanmoins, l'utilisation de ces procédés est limitée par le niveau de formabilité du matériau formé, notamment dans le cas des alliages d'aluminium. Afin d'améliorer ces limites de formabilité, des procédés de mise en forme à chaud peuvent être envisagés. L'objectif de cette thèse est d'étudier à l'aide d'approches expérimentale et numérique l'effet de la température et de la vitesse de déformation sur la formabilité des tôles en alliage d'aluminium AA5086 et de proposer une modélisation capable de prédire ces effets. Une campagne d'essais a été réalisée sur ce matériau à partir d'un essai d'emboutissage de type Marciniak. Des courbes limites de formage (CLF) ont été établies sur une plage de température allant de l'ambiant jusqu'à 200°C et pour des vitesses de déformation allant du quasi-statique à 2s-1. Des effets, positif de la température et négatif de la vitesse de déformation sur la formabilité ont été mis en évidence. La prise en compte des effets de la température et de la vitesse de déformation dans les modèles prédictifs des CLF, qu'ils soient analytiques ou numériques, est à ce jour très limitée. Dans ce travail, un modèle numérique prédictif basé sur la simulation par éléments finis du modèle géométrique de Marciniak et Kuczynski (M-K) est proposé. Les déformations limites obtenues avec de ce modèle sont très sensibles à la description du comportement thermo-viscoplastique du matériau et à la calibration du défaut géométrique pilotant l'apparition de la striction dans le modèle M-K. Des essais de traction uniaxiale réalisés dans les mêmes conditions opératoires que les essais de mise en forme de Marciniak ont permis d'identifier des lois d'écrouissage de nature très différentes (rigidifiante, saturante ou mixte). Ces lois conduisent à des prédictions très différentes de la formabilité du matériau pour une valeur donnée du défaut géométrique du modèle EF M-K. Différentes stratégies de calibration de la taille de ce défaut initial ont été envisagées. L'utilisation du point expérimental de la CLF correspondant à des conditions de déformation plane permet de calibrer de manière satisfaisante la valeur de ce défaut. Cette procédure de calibration a été appliquée pour l'ensemble des lois identifiées. Les lois de nature rigidifiante de type Ludwick se sont montrées les plus effficaces alors que les lois saturante de type Voce se sont avérées incapables de prédire la formabilité du matériau pour certaines conditions opératoires. Finalement, il est démontré qu'une valeur constante du défaut géométrique ne peut être retenue pour l'ensemble des conditions opératoires étudiées même si le modèle M-K s'est avéré assez efficace pour représenter l'effet de la température plutôt que celui de la vitesse de déformation.
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Abdul-Mahdi, F. S. "Tribological characteristics of coatings on aluminium and its alloys." Thesis, Brunel University, 1987. http://bura.brunel.ac.uk/handle/2438/5016.

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Hard anodising on aluminium and its alloys has been widely practised for many years in order to improve the resistance of the otherwise poor wear characteristics of aluminium. In recent years there has been an increasing interest in other treatments and coatings, on both aluminium and other base metals. The aim of this investigation is to explain the tribological performance and wear mechanism(s) of an uncoated aluminium alloy, four anodic coated alloys, and also an electroless nickel alloy. All of the coatings are produced on three different aluminium alloys. The thickness of the anodic films is 30-35 micron, as this thickness falls within the range commonly used by industry. In an endeavour to explain the role of coating thickness on wear life, electroless nickel alloy has been produced in a range of thicknesses of 10, 20 and 30 micron. To evaluate abrasive and adhesive wear, the samples were rubbed against a single point diamond and steel ball, respectively, in a reciprocating movement at room temperature and 65-75% relative humidity, under a wide range of load and sliding distance. Some tests continued to run until a breakdown of the coatings occurred, whilst other tests were interrupted at intermediate stages. This enabled the initiation and propagation of failure mechanisms to be studied. Abrasive wear was performed under dry conditions, whereas, adhesive wear was evaluated under both dry and lubricated conditions. Wear of these coatings was proportional to the applied load and sliding distance, but there was no direct relationship between wear and hardness. The tribological performance of these coatings appears to be dictated by a) the composition of the substrate, b) the chemical and physical nature of the coatings and c) the test conditions. Under boundary lubricated conditions there was a considerable increase in the wear life of the coatings. A three dimensional surface texture is superior to a machined surface, in controlling contact conditions. There is an approximate linear relationship between coating thickness and wear life for electroless nickel alloys. These coatings predominantly fail by adhesion, plastic deformation and brittle fracture. A microscopic model for fracture of brittle materials, under both static and dynamic conditions for abrasive and adhesive wear correlates very well with the behaviour of these coatings. Analytical interpretation of adhesive wear was made by separately calculating the coefficient of wear "K" of the counterbodies. This information enables an improved understanding of the wear test itself to be added to the model of the wear mechanisms involved.
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Bland, Marc Thompson. "Investigation of superplastic behavior in FSP 5083 aluminum alloy." Thesis, Monterey, Calif. : Naval Postgraduate School, 2007. http://bosun.nps.edu/uhtbin/hyperion-image.exe/07Jun%5FBland.pdf.

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Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2007.
Thesis Advisor(s): McNelley, Terry R. ; Su, Jianqing. "June 2007." Description based on title screen as viewed on November 7, 2007. Includes bibliographical references (p. 47-48). Also available in print.
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Balasundaram, Arunkumar. "Effect of stress state and strain on particle cracking damage evolution in 5086 wrought al-alloy." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/14809.

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Maestas, Tracy A. "Study of processing and microstructure of a superplastic 5083 aluminum alloy." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02Mar%5FMaestas.pdf.

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Wu, Weidong Aerospace &amp Mechanical Engineering Australian Defence Force Academy UNSW. "Fatigue crack propagation behaviour of welded and weld repaired 5083 aluminium alloy joints." Awarded by:University of New South Wales - Australian Defence Force Academy. School of Aerospace and Mechanical Engineering, 2002. http://handle.unsw.edu.au/1959.4/38663.

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Welding, as one of the most effective joining methods for metals, has been extensively applied in engineering usage for a long time. When cracks occur in the vicinity of weldments, weld repairs are frequently considered for crack repair to extend service life. In order to evaluate to what extent the weld repair has improved the fatigue life of a cracked welded structure, it is necessary to be able to determine the residual life of the cracked welded joint, as well as the life of the weld repaired joint. Both these assessments require that the fatigue crack growth data be available. The determination of crack propagation rates of welded and weld repaired structures is thus of paramount importance to implement a damage tolerant approach to structural life extension. However, since most studies on welded joints so far have concentrated on fatigue life evaluation, at the present time only limited information is available on crack propagation rates in welded joints, and virtually none on fatigue behaviour and crack propagation in weld repaired joints. This thesis has focused on examination of fatigue and crack propagation behaviour in as welded and weld repaired aluminium alloy 5083, a weldable marine grade alloy extensively used in construction of high speed ferries and aerospace structures. Crack growth rates were measured during constant amplitude fatigue testing on unwelded, as-welded and weld repaired specimens of 5083-H321 aluminium alloy. A 3-D finite element analysis was conducted to determine the stress intensity factors for different lengths of crack taking into account the three-dimensional nature of the weld profile. The effects of crack closure due to weld residual stresses were evaluated by taking measurements of the crack opening displacements and utilised to determine the effective stress intensity factors for each condition. Metallurgical examinations and fractography of the fracture surface were conducted using an optical microscope and SEM. It was found that crack growth rates in welded plates are of the same order of magnitude as those of parent material when effective stress intensity factors were applied. However weld repaired plates exhibit higher crack growth rates compared to those of unwelded and once-only welded plates.
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Winsley, Robert. "Corrosion resistance of heat treated and friction stir welded aluminium alloy 5083-H116." Thesis, University of Birmingham, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.713399.

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Boydon, Juanito F. "Study of cavitation and failure mechanisms of a superplastic 5083 aluminum alloy." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion/05Mar%5F.pdf.

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Harrell, James William. "Analysis of the transition in deformation mechanisms in superplastic 5083 aluminum alloys by orientation imaging microscopy /." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://sirsi.nps.navy.mil/uhtbin/hyperion-image/01Sep%5FHarrell.pdf.

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Books on the topic "5086 aluminium alloy"

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Study of Processing and Microstructure of a Superplastic 5083 Aluminum Alloy. Storming Media, 2002.

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Study of Mechanical Properties and Microstructure of Friction Stir Welded 5083 Aluminium Alloy. India: Association of Scientists, Developers and Faculties, 2014.

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Analysis of the Transition in Deformation Mechanisms in Superplastic 5083 Aluminum Alloys by Orientation Imaging Microscopy. Storming Media, 2001.

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Book chapters on the topic "5086 aluminium alloy"

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Zhao, Shasha, Rehan Qayyume, Haoyan Diao, Chaoli Ma, Xiaowei Wu, and Yong Wang. "Investigation of Superplasticity in Aluminum Alloy 5083." In ICAA13: 13th International Conference on Aluminum Alloys, 825–30. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch122.

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Zhao, Shasha, Rehan Qayyume, Haoyan Diao, Chaoli Ma, Xiaowei Wu, and Yong Wang. "Investigation of Superplasticity in Aluminum Alloy 5083." In ICAA13 Pittsburgh, 825–30. Cham: Springer International Publishing, 2012. http://dx.doi.org/10.1007/978-3-319-48761-8_122.

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Forcellese, A., L. Fratini, F. Gabrielli, and F. Micari. "Sheet Bending Modelling for AA 5083 Aluminium Alloy." In Proceedings of the Thirty-First International Matador Conference, 377–82. London: Macmillan Education UK, 1995. http://dx.doi.org/10.1007/978-1-349-13796-1_57.

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Dai, Qingsong, Yunlai Deng, Lingying Ye, Xu Liu, and Weihua Zhao. "Static Recrystallization Grain Size Model of 5083 Aluminum Alloy." In High Performance Structural Materials, 361–67. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-0104-9_37.

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Magee, Andrew, and Leila Ladani. "Mechanical Characterization of Bimodal Grain Size Aluminum 5083 under Various Test Conditions." In ICAA13: 13th International Conference on Aluminum Alloys, 1767–71. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch264.

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Walter, Timothy, Heather Murdoch, Paul Moy, Denise Yin, and Julia Cline. "High Rate Mechanical Characterization of Sensitized 5083-H131 Aluminum Alloy." In Dynamic Behavior of Materials, Volume 1, 185–87. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-30021-0_32.

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Topping, Troy D., and Enrique J. Lavernia. "Strain Hardening, Strain Softening and the Portevin-Le Chatelier Effect in Cryomilled, Ultrafine Grained AA 5083." In ICAA13: 13th International Conference on Aluminum Alloys, 959–68. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch144.

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Takaai, T., A. Daitoh, Y. Nakamura, and Y. Nakayama. "Plastic Deformation and Fracture of Continuously Cast 5083 Aluminum Alloy Ingot." In Mechanical Behavior of Materials, 313–19. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-1968-6_36.

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Chen, Y., S. W. Case, and B. Y. Lattimer. "Creep Damage Quantification and Post-fire Residual Strength of 5083 Aluminum Alloy." In Fracture, Fatigue, Failure, and Damage Evolution, Volume 5, 89–98. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-06977-7_12.

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Hirata, Tomotake, T. Oguri, H. Hagino, Tsutomu Tanaka, Chung Sung Wook, Masato Tsujikawa, Yorinobu Takigawa, and Kenji Higashi. "Formability of Friction Stir Welded and Arc Welded 5083 Aluminum Alloy Sheets." In Engineering Plasticity and Its Applications, 1473–78. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-433-2.1473.

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Conference papers on the topic "5086 aluminium alloy"

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Okon, P., G. Dearden, K. Watkins, M. Sharp, and P. French. "Laser welding of aluminium alloy 5083." In ICALEO® 2002: 21st International Congress on Laser Materials Processing and Laser Microfabrication. Laser Institute of America, 2002. http://dx.doi.org/10.2351/1.5065620.

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Boteler, J. Michael, Dattatraya P. Dandekar, Mark Elert, Michael D. Furnish, Ricky Chau, Neil Holmes, and Jeffrey Nguyen. "DYNAMIC RESPONSE OF 5083-H131 ALUMINUM ALLOY." In SHOCK COMPRESSION OF CONDENSED MATTER - 2007: Proceedings of the Conference of the American Physical Society Topical Group on Shock Compression of Condensed Matter. AIP, 2008. http://dx.doi.org/10.1063/1.2833112.

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Xu, Kang, and Mahendra D. Rana. "Pressure Temperature Ratings of Aluminum Alloy Flanges." In ASME 2018 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/pvp2018-84076.

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ASME B31.3 Appendix L provides the pressure and temperature ratings of forged aluminum flanges. The flanges are from NPS 1/2 to NPS 24 in three rating Classes 150, 300 and 600 with two grades of aluminum alloys: ASTM B247 3003-H112 and 6061-T6. However, B31.3 does not provide any technical information on the basis of the pressure and temperature ratings. A review of the historical development of ASME B16.5 indicated that the aluminum flanges had the same technical basis for pressure and temperature ratings as the ferrous alloy flanges in ASME B16.5. The 1960 Addenda of the 1957 Edition B16.5 included both aluminum flanges and ferrous alloy flanges. A new Code Case 2905 has been recently approved to allow B31.3 Appendix L aluminum flanges in fabricating Section VIII Division 1 pressure vessels as B16.5 flanges on the basis that both flange specifications have the same safety margin. In this paper, the technical basis of the pressure and temperature rating of aluminum flanges is revisited. Based on the same principle, the pressure ratings are extended to Class 900 and Class 1500 for the two aluminum alloys using the same analysis. Since ASTM B247 5083-H112 is another common grade of aluminum forging alloy, the pressure and temperature ratings are proposed for 5083-H112.
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Morette, M., Marc Dupont, and Jean-Pierre Rozelot. "Interest in aluminum alloy 5083 for telescope mirrors." In Metal Mirrors, edited by Richard G. Bingham and David D. Walker. SPIE, 1993. http://dx.doi.org/10.1117/12.158738.

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Grünenwald, S., V. Kujanpää, and A. Salminen. "Nd:YAG laser welding of 5083 aluminium alloy using filler wire." In ICALEO® 2007: 26th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2007. http://dx.doi.org/10.2351/1.5060979.

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Pleta, Abram D., Matthew C. Krugh, Chetan Nikhare, and John T. Roth. "An Investigation of Anisotropic Behavior on 5083 Aluminum Alloy Using Electric Current." In ASME 2013 International Manufacturing Science and Engineering Conference collocated with the 41st North American Manufacturing Research Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/msec2013-1244.

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Due to more stringent environmental regulations, the demand for strong, lightweight metal alloys, such as AA 5083, has increased. In sheet metal forming, aluminum is preferred over higher density steels to manufacture such parts; however the in-plane anisotropic behavior of AA 5083 alloy greatly affects its formability. Previous researchers have found that mechanical properties of metallic materials can be influenced by DC electrical current, a research area known as Electrically-Assisted Manufacturing (EAM). The research herein is focused on characterizing the in-plane anisotropic behavior of AA 5083 alloy with and without DC current application, while it is loaded in the uniaxial direction. Furthermore, the effects of EAM on Lueder’s banding will also be investigated.
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Summers, P. T., R. D. Matulich, Scott W. Case, and Brian Lattimer. "Post-Fire Mechanical Properties and Hardness of 5083 and 6082 Aluminum Alloys." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-88175.

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Aluminum alloys are being increasingly used in lightweight transportation applications such as naval vessels and passenger rail. The primary aluminum alloys considered are Al-Mg (5xxx) and Al-Mg-Si (6xxx) due to their mechanical strength, corrosion resistance, and weldability. A major concern in the use of aluminum alloys for lightweight structural applications is fire exposure. Aluminum mechanical properties begin to significantly degrade at temperatures above 300°C. After fire exposure, structural integrity will be governed by the residual, post-fire strength of the aluminum. However, scarce data is available regarding the post-fire mechanical response. The post-fire mechanical properties were characterized for several aluminum alloys: 5083-H116, 6082-T651 plate, and 6082-T6 extrusion. The alloys were exposed to elevated temperatures in a furnace to simulate a fire environment. Tension tests were performed to determine the mechanical response of the alloys. Vickers hardness measurements were also performed on specimens exposed for varying durations and temperatures to quantify the time and temperature-dependent behavior. The observed behaviors were explained in relation to the microstructural strengthening mechanisms for each alloy. Correlations were developed between the mechanical properties and Vickers hardness indentations.
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Mahdi, Sahib, and Israa Mohammed. "Studying Corrosion Behavior of Recrystallization Treatment of AA 5083 and AA 5085 Aluminium Alloys in Tigris and Shatt Al Arab." In Proceedings of the 1st International Multi-Disciplinary Conference Theme: Sustainable Development and Smart Planning, IMDC-SDSP 2020, Cyperspace, 28-30 June 2020. EAI, 2020. http://dx.doi.org/10.4108/eai.28-6-2020.2297942.

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NAM, KI WOO, SUNG KWANG KIM, SO SOON PARK, and SEOK HWAN AHN. "NONDESTRUCTIVE CHARACTERISTICS OF 1080 AND 5083 ALUMINUM ALLOY BY ECAP." In Proceedings of the International Conference on ANDE 2007. World Scientific Publishing Company, 2008. http://dx.doi.org/10.1142/9789812793034_0042.

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Chumaevsky, A. V., A. A. Eliseev, A. V. Filippov, V. E. Rubtsov, and S. Yu Tarasov. "Tensile strength on friction stir processed AMg5 (5083) aluminum alloy." In ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES 2016: Proceedings of the International Conference on Advanced Materials with Hierarchical Structure for New Technologies and Reliable Structures 2016. Author(s), 2016. http://dx.doi.org/10.1063/1.4966320.

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Reports on the topic "5086 aluminium alloy"

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Koger, J. W. Cleaning of aluminum alloy 5083. [For welding]. Office of Scientific and Technical Information (OSTI), June 1986. http://dx.doi.org/10.2172/5636263.

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Placzankis, Brian E., Chris E. Miller, and John H. Beatty. Accelerated Corrosion Analysis of Nonchromate Conversion Coatings on Aluminum Alloys 5083, 7039, and 6061 for DoD Applications. Fort Belvoir, VA: Defense Technical Information Center, August 2001. http://dx.doi.org/10.21236/ada395925.

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Placzankis, Brian E., Chris E. Miller, and Craig A. Matzdorf. GM 9540P Cyclic Accelerated Corrosion Analysis of Nonchromate Conversion Coatings on Aluminum Alloys 2024, 2219, 5083, and 7075 Using DOD Paint Systems. Fort Belvoir, VA: Defense Technical Information Center, June 2003. http://dx.doi.org/10.21236/ada416876.

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Placzankis, Brian E., Chris E. Miller, and Craig A. Matzdorf. GM 9540P Cyclic Accelerated Corrosion Analysis of Nonchromate Conversion Coatings on Aluminum Alloys 2024, 2219, 5083, and 7075 Using DoD Paint Systems. Fort Belvoir, VA: Defense Technical Information Center, April 2003. http://dx.doi.org/10.21236/ada419831.

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