Academic literature on the topic '2219 aluminum alloy'

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Journal articles on the topic "2219 aluminum alloy"

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Rosenberg, R. A., and M. W. McDowell. "2219 Aluminum Alloy by XPS." Surface Science Spectra 2, no. 2 (1993): 113–16. http://dx.doi.org/10.1116/1.1247727.

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Gao, Qi, Zhichao Zhang, Jinlong Meng, and Xiaobo Fan. "Study on warm formability of 2219 aluminum alloy with pre-deformation." Journal of Physics: Conference Series 2879, no. 1 (2024): 012019. http://dx.doi.org/10.1088/1742-6596/2879/1/012019.

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Abstract The manufacturing process of launch vehicle storage tanks requires urgent simplification, which can be improved by forming the local features after artificial aging. Therefore, a new process of warm flanging aluminum alloys with pre-deformation was proposed to meet this requirement. The mechanical properties of 2219 aluminum alloy with pre-deformation were investigated at different temperatures using thermomechanical property testing. The deformation law of warm flanging was analyzed through simulation. The flanging limit of 2219 aluminum alloy with pre-deformation was obtained throug
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Jia, Xiang-Dong, Yi-Ning Wang, Ying Zhou, and Miao-Yan Cao. "The Study on Forming Property at High Temperature and Processing Map of 2219 Aluminum Alloy." Metals 11, no. 1 (2021): 77. http://dx.doi.org/10.3390/met11010077.

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2219 aluminum alloy is a kind of high-strength Al-Cu-Mn alloy that can be strengthened by heat treatment. Its mechanical property parameters and forming properties are greatly affected by the deformation rate, temperature and strain. Taking 2219 aluminum alloy extruded bar as the research object, the Gleeble-3500 thermomechanical simulator was used to analyze the thermal compression deformation behavior of 2219 aluminum alloy under different temperatures and strain rates. The results show that the deformation behavior of 2219 aluminum alloy under high temperatures is greatly influenced by the
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Kaibyshev, R., I. Kazakulov, D. Gromov, F. Musin, D. R. Lesuer, and T. G. Nieh. "Superplasticity in a 2219 aluminum alloy." Scripta Materialia 44, no. 10 (2001): 2411–17. http://dx.doi.org/10.1016/s1359-6462(01)00930-7.

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Qu, Wen Qing, Min Yuan Song, Jun Shan Yao, and Hai Yun Zhao. "Effect of Temperature and Heat Treatment Status on the Ductile Fracture Toughness of 2219 Aluminum Alloy." Materials Science Forum 689 (June 2011): 302–7. http://dx.doi.org/10.4028/www.scientific.net/msf.689.302.

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Through measurement of fracture toughness of 2219 aluminum alloy three-point bend specimen and observation of fracture surface and microstructure at different temperature, the influences of temperature and heat treatment status on the fracture toughness of 2219 aluminum alloy are discussed. The results show that temperature has an important influence on the fracture toughness of 2219 aluminum alloy. Compared with fracture toughness in room temperature, the fracture toughness is increased by 36% at low temperature. Heat treatment status also affects fracture toughness greatly, and fracture toug
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Li, Zhi-Xin, Yi-Long Shi, Luo-Peng Xu, and Jia-Xin Jin. "Effect of Natural Aging on Cold Forming Performance of 2219 Aluminum Alloy." Materials 16, no. 9 (2023): 3536. http://dx.doi.org/10.3390/ma16093536.

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To facilitate the manufacturing of the thin-walled components of 2219 aluminum alloy, the quenching–forming–aging (Q–F–A) process has been increasingly utilized. However, natural aging (NA) after quenching significantly affects the cold forming performance of this alloy. In this study, experiments are conducted to investigate the effect of NA time on the cold forming performance of 2219 aluminum alloy. The results indicate that NA can weaken the Portevin–Le Chatelier (PLC) effect, thereby reducing its influence on the cold forming performance of the alloy. The PLC effect becomes indistinct whe
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He, Fengyang, Xu Ma, Ke Ma, Yanhong Ding, Guoming Shi, and Chengwu Wang. "Multi-Scale Simulation of Recrystallization during Rolling of Large 2219 Aluminum Alloy Rings." Metals 13, no. 3 (2023): 448. http://dx.doi.org/10.3390/met13030448.

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2219 aluminum–copper alloy is a major material in launch vehicles transition rings. The study of dynamic recrystallization during its rolling and forming process is beneficial to improving the performance enhancement of 2219 aluminum alloy ring parts. In this paper, a multi-scale simulation of grain refinement and distribution of dynamic recrystallization (DRX) grains during the rolling of 2219 aluminum alloy rings is carried out using the finite element method and cellular automata method. On the basis of the JMK DRX model, an ABAQUS subroutine was written to simulate the ring-rolling of 2219
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Lin, Haiyan, Xianchang Mao, Tugan Lin, and Jun Wei. "Second phase strengthening mechanism of 2219 aluminum alloy." Advances in Engineering Technology Research 8, no. 1 (2023): 720. http://dx.doi.org/10.56028/aetr.8.1.720.2023.

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Second phase particles have a decisive role in strengthening 2219 aluminum alloy, so it is important to study its strengthening mechanism. The different characteristics of the second phase particles of 2219 aluminum alloy were summarized, and the strengthening mechanism of deformable second phase particles (strain strengthening, chemical strengthening, order strengthening, modulus strengthening) and non-deformable second phase particles was analyzed. The strengthening mechanism model was established, the main application of the two particles was explained, and the guiding significance of the s
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Wang, Qingqing, Ningsong Qu, and Jiajie Chen. "Anodic Electrochemical Behaviors of 2219 Aluminum Alloy in NaNO3 and NaCl Electrolytes." Journal of The Electrochemical Society 171, no. 6 (2024): 062506. http://dx.doi.org/10.1149/1945-7111/ad576c.

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Because to its exceptional performance, 2219 aluminum alloy is extensively employed in the aerospace sector for large thin-wall structures. However, the machining of such structures commonly results in issues like chatter and deformation, making electrochemical machining (ECM) the preferred method. The primary focus of ECM for anode materials involves understanding their behavior during the electrochemical dissolution process. The anode electrochemical behavior of 2219 aluminum alloy in 10 wt% NaNO3 electrolyte and 10 wt% NaCl electrolyte is reported for the first time. Passivation-related cha
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Cao, Guanglong, Cheng Huang, Tong Li, Yahui Zhang, and Mingfa Ren. "Mechanical Characterization of 2219 Aluminum Alloy Welded Joints Under Bi-Axial Loading." International Journal of Applied Mechanics 11, no. 08 (2019): 1950077. http://dx.doi.org/10.1142/s1758825119500777.

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The mechanical performances of welded joints under bi-axial loading are significant to the reliability of various engineering structures. However, the protocol for the mechanical characterization of welded joints still needs to be improved to represent the mechanical performances of welded joints under complex loading conditions. In this work, an experimental design is proposed for the mechanical characterization of 2219 aluminum alloy welded joints. The target is to investigate the effects of combined tensile-shear load on the mechanical responses and failure behavior of 2219 aluminum alloy w
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Dissertations / Theses on the topic "2219 aluminum alloy"

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Yang, Haoliang. "Creep age forming investigation on aluminum alloy 2219 and related studies." Thesis, Imperial College London, 2013. http://hdl.handle.net/10044/1/39352.

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By the middle of the 20th Century, traditional mechanical metal forming methods were showing to be inadequate for producing components comprising of large high strength aluminium alloy panels with complex curvatures, such as those used in modern aircraft and aerospace metal structures. To deal with this problem, a new forming method was conceived by Textron, which has proven to be very useful for forming components with these shape characteristics and good mechanical properties. The method is called Creep Age Forming (CAF). The research described in this thesis is a study of CAF of a 2219 alum
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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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Le, Guyader Christophe. "Mécanique de la rupture et endommagement d’un alliage d’aluminium 2219 T87 pour application aérospatiale." Thesis, Paris, ENMP, 2014. http://www.theses.fr/2014ENMP0046/document.

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L'objectif de ce travail est la mise en oeuvre de la mécanique de la rupture et d'un modèle d'endommagement afin de vérifier l'intégrité du réservoir cryotechnique d'ARIANE 5 en présence de défauts. Ces derniers sont généralement assimilés à des fissures surfaciques semi-elliptiques. L'approche globale basée sur l'analyse FAD fournit une prédiction trop conservative lorsque cette méthode utilise le facteur d'intensité K et la ténacité KIc. Ce conservatisme peut toutefois être partiellement levé à condition d'introduire la notion d'intégrale J et d'utiliser une ténacité dérivée de la courbe JR
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Chen, Chih-Chang. "Evaluation of weld solidification cracking in aluminum alloys A1- 2219 and A1-2090 using the Gleeble 1500 system /." The Ohio State University, 1991. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487687115924536.

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Tardelli, Joffrey. "Etude du comportement électrochimique des phases intermétalliques des alliages d'aluminium 2214-T6 et 7050-T74 : approche multi-échelle de matériaux polyphasés." Thesis, Université de Lorraine, 2012. http://www.theses.fr/2012LORR0082/document.

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L'étude du comportement électrochimique des phases intermétalliques Al2Cu, Al2CuMg, Al7Cu2Fe, (Al,Cu)16Mn4Si3 et MgZn2, caractéristiques des alliages d'aluminium 2214-T6 et 7050-T74 et réalisée à partir d'échantillons massifs synthétisés, a montré que la formation de défauts majeurs dans la couche d'oxyde, obtenue par anodisation des alliages en milieu H2SO4 200 g/l, était directement due à la présence de ces particules au sein des alliages. L'important dégagement gazeux d'oxygène qui se produit à la surface de ces particules lors de l'étape d'anodisation explique la formation de trous et de f
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LI, ZHE-ZHI, and 李哲志. "Welding characteristic of high strongth aluminum alloy 2219." Thesis, 1989. http://ndltd.ncl.edu.tw/handle/77820043990622261188.

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Srivastava, Avanish Kumar. "Studies On Rapidly Solidified Al-Mn-Cr-Si And Al-Fe-V-Si Alloys : Processing - Microstructure Correlation." Thesis, 1995. https://etd.iisc.ac.in/handle/2005/2249.

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Srivastava, Avanish Kumar. "Studies On Rapidly Solidified Al-Mn-Cr-Si And Al-Fe-V-Si Alloys : Processing - Microstructure Correlation." Thesis, 1995. http://etd.iisc.ernet.in/handle/2005/2249.

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Nagarajan, R. "Metastable And Nanostructured Titanium-Nickel And Titanium-Nickel-Aluminium Alloys." Thesis, 1995. https://etd.iisc.ac.in/handle/2005/2215.

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Nagarajan, R. "Metastable And Nanostructured Titanium-Nickel And Titanium-Nickel-Aluminium Alloys." Thesis, 1995. http://etd.iisc.ernet.in/handle/2005/2215.

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Books on the topic "2219 aluminum alloy"

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Dawicke, D. S. Biaxial testing of 2219-T87 aluminum alloy using cruciform specimens. National Aeronautics and Administration, Langley Research Center, 1997.

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National Aeronautics and Space Administration (NASA) Staff. Biaxial Testing of 2219-T87 Aluminum Alloy Using Cruciform Specimens. Independently Published, 2018.

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Corrosion studies of 2195 Al-Li alloy and 2219 Al alloy with differing surface treatments. National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

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Book chapters on the topic "2219 aluminum alloy"

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Kaibyshev, R., O. Sitdikov, I. Mazurina, and D. R. Lesuer. "Deformation Behavior of a 2219 Aluminum Alloy." In Creep and Fracture of Engineering Materials and Structures: Proceedings of the 9th International Conference: Proceedings of the 9th International Conference, 9th ed. CRC Press, 2024. http://dx.doi.org/10.1201/9781003580089-31.

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Jian, Ningning, Lihua Chai, Zhilong Chang, et al. "The Correlation Between Structure and Performance of Advanced 2219 Aluminum Alloy." In High Performance Structural Materials. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-0104-9_21.

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Mazurina, I., Oleg Sitdikov, Rustam Kaibyshev, Hiromi Miura, and Taku Sakai. "Effect of Deformation Temperature on Microstructure Evolution in 2219 Aluminum Alloy during ECAP." In Materials Science Forum. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-443-x.545.

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Sampath, V., and N. R. Rajasekaran. "Effect of In-Situ Titanium Boride Particle Addition and Friction Stir Processing on Wear Behavior of Aluminum Alloy 2219." In Advanced Composites for Aerospace, Marine, and Land Applications II. John Wiley & Sons, Inc., 2015. http://dx.doi.org/10.1002/9781119093213.ch6.

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Sampath, V., and N. R. Rajasekaran. "Effect of In-Situ Titanium Boride Particle Addition and Friction Stir Processing on Wear Behavior of Aluminum Alloy 2219." In Advanced Composites for Aerospace, Marine, and Land Applications II. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-48141-8_6.

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Naresh, A., K. Veera Venkata Nagaraju, G. Venkatesh, and B. Vijaya Kumar. "Friction-Stir-Surfacing (FSS) Process of Aluminum Alloy (AA6061) Coating Over Mild Steel (IS2062) Substrate." In Recent Advances in Mechanical Engineering, Volume 2. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-2249-5_10.

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Sobih, Mohamed, and Zuhair Elseddig. "Electron Beam Welding of Aluminum Alloys." In Encyclopedia of Aluminum and Its Alloys. CRC Press, 2019. http://dx.doi.org/10.1201/9781351045636-140000300.

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Aluminum alloys are the subject of increasing interest in the automotive industry, as well as the aircraft industry, aiming to reduce the weight of components and also allowing a profit in term of energy saving. In assembly process, riveting has been widely used in the aircraft industry, whereas welding seems to be available in the car industry in the case of aluminum alloys. Nevertheless, conventional fusion welding can generate defects, such as gas porosity, oxide inclusions, solidification cracking (hot tearing), reduced strength in both the weld, and heat-affected zone (HAZ), which could l
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"2219 and Alclad 2219." In Properties and Selection of Aluminum Alloys. ASM International, 2019. http://dx.doi.org/10.31399/asm.hb.v02b.a0006611.

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Wierzbinska, Malgorzata, and Jan Sieniawski. "Microstructural Changes of Al-Cu Alloys After Prolonged Annealing at Elevated Temperature." In Recent Trends in Processing and Degradation of Aluminium Alloys. InTech, 2011. http://dx.doi.org/10.5772/22195.

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Conference papers on the topic "2219 aluminum alloy"

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Walsh, Daniel, Merlin Danford, and Qiu Qiong. "The Corrosion Resistance of Aluminum 2219-T87 to Dilute Biologically Active Solutions." In CORROSION 1992. NACE International, 1992. https://doi.org/10.5006/c1992-92166.

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Aluminum 2219-T87 samples were exposed to biologically active agents found in Environmental Control and Life Support System (ECLSS) hygiene waste water. Corrosive attack was correlated to alloy composition and microstructure, the electrochemistry of the fluid media, and to the microbial population found in the hygiene water.
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Walsh, Daniel W. "The Effects of Microstructure on MIC Susceptibility in High Strength Aluminum Alloys." In CORROSION 1999. NACE International, 1999. https://doi.org/10.5006/c1999-99187.

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Abstract Aluminum alloys, and in particular Al-Li-Cu alloys are attractive to the aerospace industry. The high specific strength and stiffness of these alloys will improve lift efficiency, fuel economy, performance and increase payload capabilities of air and spacecraft. The objectives of this work were to examine the corrosion behavior of Al 2195 (UNS A92195) (Al-4Cu-1Li) and to assess the effect of welding on corrosion behavior in biologically active and in sterile waters. Al 2219 (UNS A92219) samples were used in parallel tests to provide a baseline for the data generated. In this study sam
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Kendig, M., S. Jeanjaquet, and M. Mahoney. "Electrochemical Noise Analysis of the Corrosion of Aluminum Alloys and Composites." In CORROSION 1988. NACE International, 1988. https://doi.org/10.5006/c1988-88383.

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Abstract The current fluctuations between nominally identical pairs of aluminum or SiC-reinforced aluminum alloys in neutral chloride electrolytes were analyzed with respect to the time dependence, and frequency dependence of the power spectral density of the fluctuations. The results were compared to the pitting related parameters of critical potential, EC, and protection potential, Ep, obtained from potentiodynamic tests and microscopic observations. The materials examined included Al 7075-T73, Al 3003, Al 2024, Al 8090, SiC -reinforced 2124 and 2219 and a fine grain superplastic 7064 materi
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Bolling, Denzell, Adewale Olasumboye, and Gbadebo Owolabi. "Dynamic Failure of Aluminum Alloy 2219-T8 Under High Strain Rate." In ASME 2015 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/imece2015-53031.

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The suitability of aluminum alloys in a vast majority of engineering applications forms the basis for the need to understand the mechanisms responsible for their deformation and failure under various loading conditions. The material investigated in this study is AA 2219-T8 aluminum alloy. Supplied by the NASA Research Center, with high strength to weight ratio and corrosive resistance. Containing a unique mixture of aluminum, copper, and other trace elements, this alloy has potential applications in multiple fields including aerospace, defense, and commercial industries. In this paper, the dyn
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Zhang, Ping, Xiao Yu, Yuanyuan Li, and Youqiang Wang. "Research of Damage Evolution of 2219 Aluminum Alloy Weld Hole Based on ANSYS." In 2017 International Conference on Material Science, Energy and Environmental Engineering (MSEEE 2017). Atlantis Press, 2017. http://dx.doi.org/10.2991/mseee-17.2017.26.

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Shrestha, Rakish, Joseph A. Ronevich, Thorsten Michler, and Chris San Marchi. "Fatigue and Fracture Behavior of Aluminum Alloys in Gaseous Hydrogen." In ASME 2023 Pressure Vessels & Piping Conference. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/pvp2023-106442.

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Abstract Fatigue and fracture properties of aluminum alloys do not appear to degrade in the presence of dry gaseous hydrogen, based on limited available data. However, more data are needed, particularly at higher hydrogen pressure and for higher strength grades, to reliably suggest broader use of aluminum alloys for hydrogen applications. In this study, we investigate the effect of gaseous hydrogen on fatigue and fracture behavior of four aluminum alloys: 5083, 2219, 7050, and 7475. Fatigue crack growth behavior of these alloys is investigated in air and in gaseous hydrogen at pressure of 1,00
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Pacejs, Antons, Emil Yankov, Imants Adijans, Edmunds Teirumnieks, and Lyubomir Lazov. "Modification of Aluminum 1050 and 2219 Alloys Using CuBr Nanosecond Laser for Hydrophobic and Hydrophilic Properties." In The 4th International Electronic Conference on Applied Sciences. MDPI, 2023. http://dx.doi.org/10.3390/asec2023-16582.

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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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Esteves, Remelisa, Ranajay Ghosh, and Seetha Raghavan. "Stress Corrosion Cracking Studies of Additively Manufactured Aluminum Alloys." In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-2289.

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Nabak Rocha, Mellanie, Leandro João da Silva, Núbia dos Santos Saad, Ruham Reis, and Tobias Morais. "Experimental analysis of cold work in an overlap joint of aluminum alloy for a wing-to-wing assembly." In 25th International Congress of Mechanical Engineering. ABCM, 2019. http://dx.doi.org/10.26678/abcm.cobem2019.cob2019-2291.

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Reports on the topic "2219 aluminum alloy"

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Kaibyshev, R. O., I. M. Safarov, and D. R. Lesuen. Microstructural Evolution in the 2219 Aluminum Alloy During Severe Plastic Deformation. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/792652.

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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. Defense Technical Information Center, 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. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada419831.

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