Relevant bibliographies by topics / Aluminum alloys – Fracture

Contents

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

Academic literature on the topic 'Aluminum alloys – Fracture'

Author: Grafiati
Published: 4 June 2021
Last updated: 29 January 2023

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Journal articles on the topic "Aluminum alloys – Fracture"

1

Shneider, G. L., L. M. Sheveleva, and V. V. Kafel'nikov. "Delayed fracture of aluminum alloys." Metal Science and Heat Treatment 41, no. 3 (1999): 109–16. http://dx.doi.org/10.1007/bf02467695.

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Kwon, Yong Nam, Kyu Hong Lee, and Sung Hak Lee. "Fracture Toughness and Fracture Mechanisms of Cast A356 Aluminum Alloys." Key Engineering Materials 345-346 (August 2007): 633–36. http://dx.doi.org/10.4028/www.scientific.net/kem.345-346.633.

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The present study aims at investigating the effects of microstructure on fracture toughness of two A356 Al alloys. These A356 alloys were fabricated by casting processes such as rheo-casting and casting-forging, and their mechanical properties and fracture toughness were analyzed in relation with microfracture mechanisms. All the cast A356 alloys contained eutectic Si particles mainly segregated along solidification cells, and the distribution of Si particles was modified by the casting-forging process. Microfracture observation results revealed that eutectic Si particles segregated along cell
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Zhao, DongSheng, TianFei Zhang, LeLe Kong, DaiFa Long, and YuJun Liu. "Effect of ER5356 Welding Wire on Microstructure and Mechanical Properties of 5083 Aluminum Alloy GTAW Welded Joint." Journal of Ship Production and Design 37, no. 03 (2021): 196–204. http://dx.doi.org/10.5957/jspd.10200026.

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Automatic gas tungsten arc welding experiments of 5083 aluminum alloy were completed, to analyze the weld microstructure and mechanical properties. The influences of welding current, travel speed, frequency, and arc length on weld forming and mechanical properties were studied. When the welding current was 160 A, the travel speed was 380 mm/min, the frequency was 100 Hz, the arc length was 4 mm, and the maximum tensile strength of the welded joint was 296.9 MPa, which was 86.8% of the base metal’s tensile strength. The fracture elongation was 7.8%. No porosity was formed in the weld, but there
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Grinevich, A. V., V. S. Erasov, V. V. Avtaev, and S. M. Shvets. "Sheet aluminum alloys fracture toughness definition." «Aviation Materials and Technologies», s4 (2014): 40–44. http://dx.doi.org/10.18577/2071-9140-2014-0-s4-40-44.

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Hermann, R. "Environmentally Assisted Fracture of Aluminum Alloys." CORROSION 44, no. 10 (1988): 685–90. http://dx.doi.org/10.5006/1.3584929.

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Kobayashi, T. "Strength and fracture of aluminum alloys." Materials Science and Engineering: A 286, no. 2 (2000): 333–41. http://dx.doi.org/10.1016/s0921-5093(00)00935-7.

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Kobayashi, T. "Strength and fracture of aluminum alloys." Materials Science and Engineering: A 280, no. 1 (2000): 8–16. http://dx.doi.org/10.1016/s0921-5093(99)00649-8.

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Vasudévan, A. K., and S. Suresh. "Lithium-containing aluminum alloys: cyclic fracture." Metallurgical Transactions A 16, no. 3 (1985): 475–77. http://dx.doi.org/10.1007/bf02814350.

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Siddiqui, Rafiq Ahmed, Saeed Ali Al- Araimi, and Ahmet Turgutlu. "Influence of Aging Conditions on Fatigue Fracture Behaviour of 6063 Aluminum Alloy." Sultan Qaboos University Journal for Science [SQUJS] 6, no. 1 (2001): 53. http://dx.doi.org/10.24200/squjs.vol6iss1pp53-60.

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Aluminum - Magnesium - Silicon (Al-Mg-Si) 6063 alloy was heat-treated using under aged, peak aged and overage temperatures. The numbers of cycles required to cause the fatigue fracture, at constant stress, was considered as criteria for the fatigue resistance. Moreover, the fractured surface of the alloy at different aging conditions was evaluated by optical microscopy and the Scanning Electron Microscopy (SEM). The SEM micrographs confirmed the cleavage surfaces with well-defined fatigue striations. It has been observed that the various aging time and temperature of the 6063 Al-alloy, produce
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Yang, Yu Lan, Wei Qi Wang, Feng Li Li, Wei Qing Li, and Yong Qiang Zhang. "The Effect of Aluminum Equivalent and Molybdenum Equivalent on the Mechanical Properties of High Strength and High Toughness Titanium Alloys." Materials Science Forum 618-619 (April 2009): 169–72. http://dx.doi.org/10.4028/www.scientific.net/msf.618-619.169.

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The effect of Aluminum equivalent and Molybdenum equivalent on the strength and fracture toughness of titanium alloys was studied in this paper. The result shows that the tensile strength of the alloy increases with increasing of aluminum equivalent and molybdenum equivalent and the fracture toughness decreases gradually, the effect of aluminum equivalent is comparatively more conspicuous. A suitable value range of aluminum equivalent and molybdenum equivalent of high strength and high toughness titanium alloys are obtained from the analysis, based on this, a new type of high strength and high
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Dissertations / Theses on the topic "Aluminum alloys – Fracture"

1

Lee, Jonghee. "Fracture analysis of a propagating crack in a ductile material /." Thesis, Connect to this title online; UW restricted, 1996. http://hdl.handle.net/1773/7081.

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Zafari, Farzad. "Experimental and numberical study of elastic-plastic mixed-mode fracture /." Thesis, Connect to this title online; UW restricted, 1997. http://hdl.handle.net/1773/7034.

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Pouillier, Édouard. "Hydrogen-induced Intergranular Fracture of Aluminum-Magnesium Alloys." Paris, ENMP, 2011. http://www.theses.fr/2011ENMP0095.

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Les alliages d'aluminium de la famille 5XXX (Al-Mg) sont utilisés dans la fabrication de pièces de structure en raison de leurs bonnes propriétés mécaniques, de soudabilité et de résistance à la corrosion. Toutefois, dans des conditions d'utilisation sévères, une synergie entre la déformation plastique et les réactions de corrosion se produit et entraîne une fissuration intergranulaire, par corrosion sous contrainte (CSC), voire par fragilisation par l'hydrogène (FPH). La ductilité passe de 50% à quelques %, montrant une fissuration fragile. La compréhension des mécanismes qui régissent ce typ
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Lyons, Jed S. "Microstructural influences on fracture toughness in A357 cast aluminum alloys." Thesis, Georgia Institute of Technology, 1987. http://hdl.handle.net/1853/16689.

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Deshpande, Nishkamraj U. "Characterization of fracture path and its relationship with microstructure and fracture toughness of aluminum alloy 7050." Diss., Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/20210.

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Jordon, James Brian. "EXPERIMENTS AND MODELING OF FATIGUE AND FRACTURE OF ALUMINUM ALLOYS." MSSTATE, 2008. http://sun.library.msstate.edu/ETD-db/theses/available/etd-11062008-110529/.

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In this work, understanding the microstructural effects of monotonic and cyclic failure of wrought 7075-T651 and cast A356 aluminum alloys were examined. In particular, the structure-property relations were quantified for the plasticity/damage model and two fatigue crack models. Several types of experiments were employed to adapt an internal state variable plasticity and damage model to the wrought alloy. The damage model was originally developed for cast alloys and thus, the model was modified to account for void nucleation, growth, and coalescence for a wrought alloy. In addition, fatigue ex
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Vasudevan, Satish. "AN INVESTIGATION OF QUASI-STATIC BEHAVIOR, HIGH CYCLE FATIGUE AND FINAL FRACTURE BEHAVIOR OFALUMINUM ALLOY 2024 AND ALUMINUM ALLOY 2219." Akron, OH : University of Akron, 2007. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=akron1193668130.

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Thesis (M.S.)--University of Akron, Dept. of Mechanical Engineering, 2007.<br>"December, 2007." Title from electronic thesis title page (viewed 02/23/2008) Advisor, T. S. Srivatsan; Faculty readers, Craig Menzemer, Amit Prakash; Department Chair, Celal Batur; Dean of the College, George K. Haritos; Dean of the Graduate School, George R. Newkome. Includes bibliographical references.
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Dadkhah, Mahyar Sh. "Analysis of ductile fracture under biaxial loading using moiré interferometry /." Thesis, Connect to this title online; UW restricted, 1988. http://hdl.handle.net/1773/7026.

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Hilty, Eric. "Influence of Welding and Heat Treatment on Aluminum Alloys." University of Akron / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=akron1396877051.

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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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Books on the topic "Aluminum alloys – Fracture"

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Fracture resistance of aluminum alloys: Notch toughness, tear resistance, and fracture toughness. Aluminum Association, 2001.

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2

Beaver, P. W. Experimental and theoretical determination of J(IC) for 2024-T351 aluminium alloy. Aeronautical Research Laboratories, 1986.

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Schwarmann, L. Material data of high-strength aluminium alloys for durability evaluation of structures: Fatigue strength, crack propagation, fracture toughness. Aluminium-Verlag, 1986.

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4

Gross, Jürgen. Eigenschaften von Aluminium-Silicium-Legierungen in unterschiedlichen Behandlungszuständen unter besonderer Beachtung des Gefügeeinflusses auf die Festigkeitswerte und auf das Bruchverhalten. Wissenschaft und Technik Verlag, 1992.

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1950-, Cheng Shu-hong, and Mobley Carroll E. 1941-, eds. A fractography atlas of casting alloys. Battelle Press, 1992.

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Wanhill, R. J. H. Fatigue and fracture of aerospace aluminium alloys: A short course. National Aerospace Laboratory, 1994.

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Höhne, Volker. Mechanische und bruchmechanische Bewertung des Bruchverhaltens von WIG-Schweissverbindungen der Aluminiumlegierung A1Mg4,5Mn bei statischer, dynamischer und zyklischer Beanspruchung. Deutscher Verlag für Grundstoffindustrie, 1991.

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Materials Solutions Conference 2001 (2001 Indianapolis, Ind.). Advances in the metallurgy of aluminum alloys: Proceedings from Materials Solutions Conference 2001 : the James T. Staley honorary symposium on aluminum alloys, 5-8 November 2001, Indianapolis, Indiana. ASM International, 2001.

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Idziak, Adam. Anizotropia prędkości fal sejsmicznych i jej związek z orientacją systemów spękań masywów skalnych. Uniwersytet Śląski, 1992.

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Koning, A. V. de. Finite element analyses of stable crack growth in thin sheet material. National Aerospace Laboratory, 1985.

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Book chapters on the topic "Aluminum alloys – Fracture"

1

Toda, Hiroyuki, Hideyuki Oogo, Hideki Tsuruta, et al. "Origin of Ductile Fracture in Aluminum Alloys." In ICAA13: 13th International Conference on Aluminum Alloys. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch83.

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Toda, Hiroyuki, Hideyuki Oogo, Hideki Tsuruta, et al. "Origin of Ductile Fracture in Aluminum Alloys." In ICAA13 Pittsburgh. Springer International Publishing, 2012. http://dx.doi.org/10.1007/978-3-319-48761-8_83.

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Kwon, Yong Nam, Kyu Hong Lee, and Sung Hak Lee. "Fracture Toughness and Fracture Mechanisms of Cast A356 Aluminum Alloys." In The Mechanical Behavior of Materials X. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-440-5.633.

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Reynolds, Anthony P., Bob Wheeler, and Kumar V. Jata. "Deformation, Fracture and Fatigue in a Dispersion Strengthened Aluminum Alloy." In Lightweight Alloys for Aerospace Application. John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118787922.ch8.

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Denzer, D. K., R. J. Rioja, G. H. Bray, G. B. Venema, and E. L. Colvin. "The Evolution of Plate and Extruded Products with High Strength and Fracture Toughness." In ICAA13: 13th International Conference on Aluminum Alloys. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch86.

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Boselli, J., G. Bray, R. J. Rioja, et al. "The Metallurgy of High Fracture Toughness Aluminum-Based Plate Products for Aircraft Internal Structure." In ICAA13: 13th International Conference on Aluminum Alloys. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch85.

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Bouazara, M. "Improvement in the Design of Automobile Upper Suspension Control Arms Using Aluminum Alloys." In Damage and Fracture Mechanics. Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-2669-9_11.

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Tayon, Wesley A., Marcia S. Domack, and Stephen J. Hales. "Correlation of Fracture Behavior with Microstructure in Friction Stir Welded, and Spin-formed Al-Li 2195 Domes." In ICAA13: 13th International Conference on Aluminum Alloys. John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch90.

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Jin, Helena, Wei-Yang Lu, John Korellis, and Sam McFadden. "Experimental Study of Voids in High Strength Aluminum Alloys." In Time Dependent Constitutive Behavior and Fracture/Failure Processes, Volume 3. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9794-4_6.

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Mae, Hiroyuki, Xiaoqing Teng, Yuanli Bai, and Tomasz Wierzbicki. "Calibration of Ductile Fracture Properties of Two Cast Aluminum Alloys." In Experimental Analysis of Nano and Engineering Materials and Structures. Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6239-1_396.

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Conference papers on the topic "Aluminum alloys – Fracture"

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San Marchi, Chris, Martina Schwarz, and Joseph Ronevich. "Effect of High-Pressure Hydrogen and Water Impurity on Aluminum Alloys." In ASME 2020 Pressure Vessels & Piping Conference. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/pvp2020-21277.

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Abstract Aluminum alloys are desirable in mobile fuel cell applications due to the combination of strength, hydrogen resistance, and low density. In dry hydrogen environments, the fatigue and fracture resistance of common structural aluminum alloys are not degraded compared to air environments. However, aluminum alloys can be susceptible to stress corrosion cracking in humid air, which raises questions about the potential deleterious effects of moisture impurities in high-pressure hydrogen environments. While this study does not address the effects of the air environment on aluminum hydrogen p
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Li, Ming. "Dimensional Analysis: A Different Perspective to Design Aluminum Alloys Concerning Intergranular Fracture." In Proceedings of the International Symposium on Plasticity and Impact (ISPI 2001). WORLD SCIENTIFIC, 2001. http://dx.doi.org/10.1142/9789812794536_0014.

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Matsuoka, Saburo, Takashi Iijima, Satoko Yoshida, Junichiro Yamabe, and Hisao Matsunaga. "Various Strength Properties of Aluminum Alloys in High-Pressure Hydrogen Gas Environment." In ASME 2019 Pressure Vessels & Piping Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/pvp2019-93478.

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Abstract Three types of strength tests, slow strain rate tensile (SSRT), fatigue life, and fatigue crack growth (FCG) tests, were performed using six types of aluminum alloys, 5083-O, 6061-T6, 6066-T6, 7N01-T5, 7N01-T6, and 7075-T6, in air and 115 MPa hydrogen gas at room temperature. All the strength properties of every material were not deteriorated in 115 MPa hydrogen gas. In all the materials, FCG rates were lower in 115 MPa hydrogen gas than in air. This was considered to be due to a lack of water- or oxygen-adsorbed film at crack tip in hydrogen gas. In 5083-O, 6061-T6 and 6066-T6, relat
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Wahab, Muhammad A., and Vinay Raghuram. "Fatigue and Fracture Mechanics Analysis of Friction Stir Welded Joints of Aerospace Aluminum Alloys Al-2195." In ASME 2013 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/imece2013-63285.

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Friction-Stir-Welding (FSW) has been adopted as a major process for welding Aluminum aerospace structures. Aluminum (Al-2195) which is one of the new generations Aluminum alloys that has been used for the new super lightweight external tank for the space shuttle. NASA’s Michaud Assembly Facility (MAF) in New Orleans is continuously pursuing Friction-Stir-Welding (FSW) technologies in its efforts to advance fabrication of the external tanks of the space shuttles. The future launch vehicles which will have reusable mandates, for the structure to have good fatigue properties which prompts an inve
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Farahmand, Bob. "Fracture Properties Estimation of Aluminum Lithium Alloys Subjected to Exposure Time (Analytical Approach Versus Physical Testing)." In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-1937.

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Miscia, Giuseppe, Vincenzo Rotondella, Andrea Baldini, Enrico Bertocchi, and Luca D’Agostino. "Aluminum Structures in Automotive: Experimental and Numerical Investigation for Advanced Crashworthiness." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-51724.

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Ductility of aluminum alloys is highly used in automotive applications where crashworthiness becomes relevant. Due to its physical and mechanical properties, aluminum allows structures to be designed with good capacity to absorb energy, without increasing the overall weight of cars. In particular, high elongation allows for the conversion of a great amount of kinetic energy related to crash events in plastic deformation. If this was not the case, the energy involved during an accident could interest also the occupants, causing serious injuries. During large deformation of structures, chassis c
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Yan, Cuifen, Xin Wu, and Sayed Nassar. "Characterization of Adhesive-Bonded Sheet Metal Joints." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-63498.

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The bonding strength of metal-metal single-lap joints with different adhesives applied on steels and aluminum alloys were studied. The bonding strength is found to be related to the type of adhesives and the backing metal, the surface roughness, the surface scratch orientations, the adhesive layer thickness, and the loading conditions (static vs. cyclic and loading rate). SEM observation of fractured surfaces reveals some common feature of bonding strength enhancement, fracture paths and the mechanisms of fracture. The direction of the adhesive joint design is suggested.
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Salandro, Wesley A., Joshua J. Jones, Timothy A. McNeal, John T. Roth, Sung-Tae Hong, and Mark T. Smith. "Effect of Electrical Pulsing on Various Heat Treatments of 5XXX Series Aluminum Alloys." In ASME 2008 International Manufacturing Science and Engineering Conference collocated with the 3rd JSME/ASME International Conference on Materials and Processing. ASMEDC, 2008. http://dx.doi.org/10.1115/msec_icmp2008-72512.

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Previous studies have shown that the presence of a pulsed electrical current, applied during the deformation process of an aluminum specimen, can significantly improve the formability of the aluminum without heating the metal above its maximum operating temperature range. The research herein extends these findings by examining the effect of electrical pulsing on 5052 and 5083 Aluminum Alloys. Two different parameter sets were used while pulsing three different heat treatments (As Is, 398°C, and 510°C) for each of the two aluminum alloys. For this research, the electrical pulsing is applied to
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Sugihara, Tatsuya, Takuma Nomura, Toshiyuki Enomoto, Anirudh Udupa, Koushik Viswanathan, and James Mann. "Exploring the Role of Mechanochemical Effects in Cutting of Aluminum Alloys With Alcohols." In ASME 2022 17th International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/msec2022-85192.

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Abstract In metal cutting processes, a chemical ambient environment in the cutting zone can be a useful variable for process control and process performance improvement. In this work, we study how mechanochemical effects influence the chip formation process, especially focusing on a specific chemical reaction between aluminum alloys and alcohols as a model system. Using high speed in-situ imaging and particle image velocimetry, we demonstrate that the mechanochemical effect in cutting of annealed Al with use of isopropyl alcohol (IPA) is manifest in two different ways: a lubricating effect at
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Li, Zhuoqun, and Xin Wu. "Inner Surface Cracking of an Aluminum Alloy in Small-Radius Bending." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-42976.

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Aluminum alloys, due to their low density, high strength to weight ratio and formability, are widely used in automotive components. At present, most of the sheet alloy being used is AA6111; an Al-Mg-Si alloy with addition of Cu. AA6111. These alloys contain micrometer sized inclusions and second phase particles, with good combination of strength and formability [1]. However, at the same time, the formability of AA6111 is also limited because of these micro-sized inclusions and second phase particles [2]. To improve the formability of sheet metal used as automotive body such as panels, a newer
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Reports on the topic "Aluminum alloys – Fracture"

1

D. Schwam: J.F. Wallace: Y. Zhu: J.W. Ki. Metallic Reinforcement of Direct Squeeze Die Casting Aluminum Alloys for Improved Strength and Fracture Resistance. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/882786.

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Starke, Edgar A., and Jr. Investigation of the Role of Trace Additions of Precipitation, Deformation and Fracture on Aluminum Alloys. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada389780.

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deWit, Roland, Richard J. Fields, Samuel R. III Low, Donald E. Harne, and Tim Foecke. Fracture testing of large-scale thin-sheet aluminum alloy. National Institute of Standards and Technology, 1995. http://dx.doi.org/10.6028/nist.ir.5661.

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