Relevant bibliographies by topics / Aluminum 2024

Contents

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

Academic literature on the topic 'Aluminum 2024'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Aluminum 2024"

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Zhu, Dezhi, Zhenxing Zheng, and Qi Chen. "Strain-rate sensitivity of aluminum 2024-T6/TiB2 composites and aluminum 2024-T6." Journal of Wuhan University of Technology-Mater. Sci. Ed. 30, no. 2 (April 2015): 256–60. http://dx.doi.org/10.1007/s11595-015-1135-4.

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Nugroho, Fajar. "PENGARUH RAPAT ARUS ANODIZING TERHADAP NILAI KEKERASAN PADA PLAT ALUMINIUM PADUAN AA SERI 2024-T3." Angkasa: Jurnal Ilmiah Bidang Teknologi 7, no. 2 (September 13, 2017): 39. http://dx.doi.org/10.28989/angkasa.v7i2.147.

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Aluminum alloy AA 2024-T3 is widely applied in the aircraft industry because it has good mechanical properties such as; light weight, good conductivity and the corrosion resistance. However Aluminium 2024-T3 susceptible to wearing. One method to improve the wear resistance o f AA 2024-T3 is the anodizing process. The aims of this research to study the effect of current density and anodizing time against the hardness of aluminum alloy AA 2024-T3. The process of anodizing was carried out using 10 percent sulfuric acid solution with the current density of 1.5 Ampere per decimeters square, 3.0 Ampere per decimeters square and 4.5 Ampere per decimeters square with immersion times of 30, 40, 50 and 60 minutes. Furthermore, the surface hardness was measured by using the Vickers hardness test method. As the supporting data the composition of the test conducted, testing the microstructure, and vickers hardness test. This study shows that the surface hardness of aluminum alloy AA 2024-T3 is influenced by the current density and anodizing time with varying values. Its shows that higher current density o f the anodizing caused optimal time tends to be short. The longer anodising time it will produce greater layer of aluminum oxide.
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Zhu, De Zhi, Wei Ping Chen, and Yuan Yuan Li. "Strain-Rate Relationship of Aluminum Matrix Composites Predicted by Johnson-Cook Model." Materials Science Forum 704-705 (December 2011): 935–40. http://dx.doi.org/10.4028/www.scientific.net/msf.704-705.935.

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Strain-rate sensitivities of 55-65vol.% aluminum 2024-T6/TiB2composites and the corresponding aluminum 2024-T6 matrix were investigated using split Hopkinson pressure bar. Results showed that 55-65vol.% aluminum 2024-T6/TiB2composites exhibited significant strain-rate sensitivities, which were three times higher than that of the aluminum 2024-T6 matrix. The strain-rate sensitivity of the aluminum 2024-T6 matrix composites rose obviously with reinforcement content increasing (up to 60%), which agreed with the previous researches. The aluminum 2024-T6/TiB2composites showed hybrid fracture characteristics including particle cracking and aluminum alloy softening under dynamic loading. The flow stresses predicted by Johnson-Cook model increased slowly when the reinforcement volume fraction ranged in 10%-40%. While the reinforcement volume fraction was over 40%, the flow stresses of aluminum matrix composites increased obviously and the strains dropped sharply. Keywords: Composite materials; Dynamic compression; Stress-strain relationship
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Junipitoyo, Bambang, Luqman Hakim Al Baihaqy, and Linda Winiasri. "Pengaruh Heat Treatment Dan Quenching Terhadap Sifat Fisis Dan Mekanis Aluminum Alloy 2024-t3." Jurnal Penelitian 5, no. 1 (April 27, 2020): 1–10. http://dx.doi.org/10.46491/jp.v5e1.481.1-10.

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Aluminum alloy banyak digunakan pada industri manufaktur dirgantara sebagai material struktur pesawat terbang karena memiliki sifat yang ringan namun kuat. Aluminum alloy 2024 sering digunakan pada skin pesawat terbangPengujian yang dilakukan dengan cara Aluminum Alloy 2024-T3 di heat treatment pada suhu 100, 150 dan 200 °C dengan waktu tahan 60 menit, 90 menit dan 120 menit kemudian di quenching menggunakan air. Setelah dilakukan heat treatment dan quenching Aluminum Alloy 2024-T3 di uji tarik, uji kekerasan brinell, dan pengamatan struktur mikro dari Aluminum Alloy 2024-T3. Dari hasil penelitian ini menunjukkan bahwa heat treatment dan quenching pada Aluminum Alloy 2024-T3, diperoleh nilai tensile stress rata-rata tertinggi pada suhu 150 °C dengan waktu tahan 90 menit sebesar 154,52 Mpa, kekerasan rata-rata teringgi pada suhu 150 °C dengan waktu tahan 120 menit sebesar 95,66 HBW.
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Huang, Chuan Yong. "Electroless Ni-La-P Coatings on 2024 Aluminum Alloys for Aircraft Structure." Applied Mechanics and Materials 224 (November 2012): 348–51. http://dx.doi.org/10.4028/www.scientific.net/amm.224.348.

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2024 aluminium alloys are widely used in airframe construction.However,this series of alloys are susceptible to corrosion to limit their usefulness,In this study,electroless Ni-La-P alloy plating on aluminum alloy and the effects of pH value,temperature and concentration of LaNiO3 on deposition rate were investigated.Surface morphology and corosion-resistant of the electroless Ni-La-P deposits were evaluated.The results showed the corrosion-resistant in 5％ NaC1 solutions obviously enhance compared with original aluminum alloy using electroless Ni-La-P deposition method．
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Zhang, Shi Xing, Yu Ping Zhu, and Gang Yi Cai. "Influence of Overburning on Microstructure and Property of 2024 Aluminum Alloy." Advanced Materials Research 941-944 (June 2014): 3–7. http://dx.doi.org/10.4028/www.scientific.net/amr.941-944.3.

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Process of solution treatment of 2024 aluminum alloy was done by hardness test and microanalysis in this paper. The effects of different solution treatment temperature on the microstructure and mechanical properties of 2024 aluminum alloy were studied and the influence of overburning on the microstructure and mechanical properties of 2024 aluminum alloy were also analyzed. The experimental results show that overburning occurs while 2024 aluminum alloy is heated over 490°C×50min . The hardness tests and microstructure analysis results show that the hardness decreased, grain boundary becomes trigemanal and compounded –melting structure (burnt structure) appeared when overburning occuring for this alloy .
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Isanaka, Sriram Praneeth, Sreekar Karnati, and Frank Liou. "Blown powder deposition of 4047 aluminum on 2024 aluminum substrates." Manufacturing Letters 7 (January 2016): 11–14. http://dx.doi.org/10.1016/j.mfglet.2015.11.007.

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Anghelina, Florina Violeta, Ionica Ionita, Dan Nicolae Ungureanu, Elena Valentina Stoian, Ileana Nicoleta Popescu, Vasile Bratu, Ivona Petre, Carmen Popa, and Alexis Negrea. "Structural Aspects Revealed by X-Ray Diffraction for Aluminum Alloys 2024 Type." Key Engineering Materials 750 (August 2017): 20–25. http://dx.doi.org/10.4028/www.scientific.net/kem.750.20.

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This paper presents experimental results revealed on the samples type 2024 aluminum alloy used in aeronautics. Adequate characterization of 2024 aluminum alloys with special destination (aviation) was achieved by combined investigations:(i) wet chemical analysis, (ii) spectrochemical analysis, (iii) X-ray diffraction and (iv) electron microscopy. The main conclusion that emerges from the investigations carried out on aluminum samples revealed that: (a) alloys fits in terms of composition with the standard specification for 2024, in all cases; (b) microstructure vary in fineness of grain, but meets the requirements of aviation rules; the investigated microstructures have been appreciated as adequate of aluminum alloys type "2024".
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Mrówka-Nowotnik, Grazyna, and Jan Sieniawski. "Analysis of Intermetallic Phases in 2024 Aluminium Alloy." Solid State Phenomena 197 (February 2013): 238–43. http://dx.doi.org/10.4028/www.scientific.net/ssp.197.238.

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The main objective of this study was to analyze the evolution of the microstructure (morphology, composition and distribution of intermetallic phases) in the 2024 aluminium alloy cooled with different cooling rates after solidification process. A few techniques: optical light microscopy (LM), scanning (SEM) electron microscopy combined with an energy dispersive X-ray microanalysis (EDS), X-ray diffraction (XRD) were used to identify intermetallics in the examined alloy. The results show that the microstructure of 2024 aluminum alloys in as-cast condition consisted following intermetallic phases: Al2Cu, Al2CuMg, Al7Cu2Fe, Al4Cu2Mg8Si7, AlCuFeMnSi and Mg2Si.
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Wu, Jin Hao, You Hong Sun, Qing Nan Meng, Chi Zhang, and Su Su Peng. "Mechanical and Tribological Behaviors of WAl12 Reinforced 2024 Aluminum Alloy Matrix Composites." Materials Science Forum 993 (May 2020): 60–67. http://dx.doi.org/10.4028/www.scientific.net/msf.993.60.

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WAl12 reinforced 2024 aluminum alloy matrix composites were prepared by powder metallurgy with tungsten particles and W50Al50 alloy particles. The effects of WAl12 on the mechanical properties of 2024 aluminum alloy composites at room temperature and high temperature were studied, and the friction behavior was characterized. The results show that intermetallic WAl12 phase forms in the composite by 2024 aluminum alloy and tungsten. The mechanical properties and friction behavior can be improved by the formation of intermetallic WAl12 phase. The tensile strength of 2024 aluminum alloy at room temperature and 180 °C can be improved by adding tungsten less than 1.5 at.%. Adding 2.0 at.% tungsten can reduce the friction coefficient by 20 % and the scratch width by 40 %. The tensile fracture surface of the sample was analyzed by scanning electron microscopy (SEM), indicating that WAl12 intermetallic phase is closely connected with the aluminum matrix.
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Dissertations / Theses on the topic "Aluminum 2024"

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Cai, Hong. "Microbiologically influenced corrosion and titanate conversion coatings on aluminum alloy 2024-T3 /." View online ; access limited to URI, 2006. http://0-wwwlib.umi.com.helin.uri.edu/dissertations/dlnow/3225314.

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Akhtar, Anisa Shera. "Surface science studies of conversion coatings on 2024-T3 aluminum alloy." Thesis, University of British Columbia, 2008. http://hdl.handle.net/2429/1713.

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The research in this thesis aims to develop new mechanistic knowledge for coating processes at 2024-Al alloy surfaces, ultimately to aid the design of new protective coatings. Coatings formed by phosphating, chromating, and permanganating were characterized especially by scanning Auger microscopy (SAM), X-ray photoelectron spectroscopy, and scanning electron microscopy . The objective was to learn about growth (nm level) as a function of time for different coating baths, as well as a function of lateral position across the different surface microstructural regions, specifically on the μm-sized Al-Cu-Mg and Al-Cu-Fe-Mn particles which are embedded in the alloy matrix . The research characterizes coating thickness, composition, and morphology. The thesis emphasizes learning about the effect of different additives in zinc phosphating baths . It was found that the Ni²⁺ additive has two main roles : first, the rate of increase in local solution pH is limited by the slower kinetics of reactions involving Ni²⁺ compared to Zn²⁺, leading to thinner zinc phosphate (ZPO) coatings when Ni²⁺ is present. Second, most Ni²⁺ deposition occurs during the later stages of the coating process in the form of nickel phosphate and a Ni-Al oxide in the coating pores on the alloy surface, increasing the corrosion resistance. Aluminum fluoride precipitates first during the initial stages of the coating process, followed by aluminum phosphate, zinc oxide, and finally ZPO. When Ni²⁺ is present in the coating solution at 2000 ppm, ZnO predominates in the coating above the A-Cu-Fe-Mn particle while ZPO dominates on the rest of the surface. The Mn²⁺ additive gives a more even coating distribution (compared with Ni²⁺) across the whole surface. The Mn²⁺ -containing ZPO coating is similar to the chromate coating in terms of evenness, while there is more coating deposition at the second-phase particles for permanganate coatings. The oxides on the Al-Cu-Fe-Mn and matrix regions are similar before coating, thereby confirming that a variety of observed differences in ZPO coating characteristics at these regions arise from the different electrochemical characteristics of the underlying metals. Upon exposure to a corrosive solution, the ZPO coating provides more protection to the second-phase particles compared to the matrix.
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Wang, Xi. "Corrosion Protection of Aluminum Alloy 2024-T3 by Al-Rich Primer." The Ohio State University, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1557143060015145.

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Gujarathi, Kedar Kanayalal. "Corrosion of aluminum alloy 2024 belonging to the 1930s in seawater environment." [College Station, Tex. : Texas A&M University, 2008. http://hdl.handle.net/1969.1/ETD-TAMU-3002.

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GUO, YANG. "A Study of Trivalent Chrome Process Coatings on Aluminum Alloy 2024-T3." The Ohio State University, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=osu1308166499.

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Patel, Rishikumar M. "Investigating the Mechanical Behavior of Conventionally Processed High Strength Aluminum Alloy 2024." University of Akron / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=akron1523106869575194.

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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.
"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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Silva, José Wilson de Jesus [UNESP]. "Efeito dos oxi-ânions do grupo VIB sobre a corrosão aquosa das ligas Al(2024) e Al(7050) utilizadas na indústria aeronaútica." Universidade Estadual Paulista (UNESP), 2003. http://hdl.handle.net/11449/97122.

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Made available in DSpace on 2014-06-11T19:28:35Z (GMT). No. of bitstreams: 0 Previous issue date: 2003Bitstream added on 2014-06-13T20:37:40Z : No. of bitstreams: 1 silva_jwj_me_guara.pdf: 1820882 bytes, checksum: 7e96fbad2b277d2b628c44604b9cf46d (MD5)
Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
Foram caracterizados os comportamentos eletroquímicos e avaliadas as resistências à corrosão das ligas aeronáuticas 2024-T351 e 7050-T7451 em soluções aquosas de cloreto contendo cromato, molibdato e tungstato. Foram realizados ensaios de corrosão não-eletroquímicos de imersão prolongada acompanhados de análise metalográfica de superfície por microscopia óptica e identificação dos produtos de corrosão por difratometria de raios-X. A análise quantitativa de superfícies das ligas após a imersão, indica que os pites formados têm áreas médias similares. Os pites são mais largos do que profundos e de geometria, predominantemente, cônica ou quase-cônica e irregular. Em todos os produtos de corrosão de cada liga foi encontrado hidróxido de alumínio, em suas diferentes formas cristalinas. Medidas de perda de dureza, como uma conseqüência da deterioração superficial, também foram determinadas. Além disso, ensaios eletroquímicos como medidas de potencial em circuito aberto, curvas de polarização e voltametria cíclica complementaram este estudo. Em meio aerado os resultados obtidos mediante medidas eletroquímicas são consistentes com aqueles obtidos nos ensaios de imersão, em particular o efeito do CrO42- e do MoO42-. O WO42- mostrou-se agressivo em períodos prolongados de imersão. Apesar dos ensaios revelarem uma redução parcial de MoO42- em ambas as ligas, o efeito desse oxi-ânion parece ser diferente sobre cada liga. Em meio desaerado as ligas apresentam passivação em todos os eletrólitos. A adição dos oxi-ânions não modificou significativamente o potencial de pite para a liga 7050, enquanto que para a liga 2024 ele foi deslocado levemente para valores mais positivos.
It has been characterized the electrochemical behavior and evaluated the 2024-T351 and 7050-T7451 aircraft alloys corrosion resistance in chloride aqueous solutions containing chromate, molybdate and tungstate. It has been carried out non-electrochemical long immersion corrosion testings accompanied by surface metalography analysis achieved by light microscopy and corrosion products identification by X-ray difratometry. Surfaces quantitative analysis upon the alloys after immersion, indicates that formed pits have similar average area. Pits are widther than deeper and own predominantly a conical or quasi-conical and irregular geometry. In all corrosion products of each alloy it has been found aluminum hydroxide in its different crystalline ways. Hardness loss measurements have also been determined. In addition, electrochemical testings such as open circuit potential measures, polarization curves and cyclical voltammetry have completed this study. In aerated means the obtained results before electrochemical mesurements are similar to those obtained in the immersion tests, in particular CrO42- and MoO42- effects. WO42- has been found to be aggressive in very long immersion period. Though tests display a MoO42- partial reduction in both alloys, this oxi-anion effect seems to be different upon each alloy. In de-aerated means alloys present passivation in all eletrolytes. Oxi-anion addition has not changed significantly pit potential for 7050 alloy, while for 2024 alloy it has been dislocated, slightly, for more positive values.
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Mann, Philip. "Evaluation of surface modifications introduced by shot peening of aluminum alloy 2024-T351." Thesis, McGill University, 2014. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=123117.

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Shot peening is a cold working mechanical deformation process consisting of bombarding a metallic surface with small spherical media, called shots, at velocities commonly in the range of 10 to 100 m/s. Upon impact, the shots generate a near-surface deformed layer containing local hardening as well as compressive residual stresses, resulting in an improved fatigue resistance. However, the dependence of shot velocity and percentage of the total area covered by shot impacts on the surface modification introduced by shot peening are not well understood.The hardness and residual stress profiles beneath shot peened surfaces were investigated using nanoindentation experiments for the situations of three different average shot velocities, corresponding to 35 m/s, 54 m/s and 66 m/s, and two surface coverages, corresponding to a single shot peening impingement and full coverage (100%). For the situation (i) of a single impingement, a new polishing procedure was developed allowing locating an isolated single impingement, verifying that the impingement was produced by a shot that impacted at normal incidence, as well as preparing the surface such that nanoindentation could be performed on the impingement's cross-section. It was demonstrated that both hardness and compressive residual stresses increased with an increase in shot velocity. The experimental residual stress results were compared to those from numerical simulations that utilized the same peening parameters as the experiments. It was observed that the experimental results demonstrated similar behavior and were of the same order of magnitude as those predicted numerically. The main difference was that the experimental results demonstrated a maximum compressive residual stress that was independent of shot velocity.For the situation (ii) of full coverage, channelling contrast imaging in a scanning electron microscope revealed that there were recrystallized grains adjacent to the shot peened edge. Additionally, the hardness and compressive residual stresses were observed to increase with an increase in shot velocity. Similarly to the single impingement, the location of maximum compressive residual stress was independent of shot velocity.
Le grenaillage est un procédé de déformation mécanique consistant à bombarder une surface métallique ductile avec de petits billes sphériques à des vitesses élevées (10 à 100 m/s). Lors de l'impact, les billes génèrent l'apparition d'une zone déformée en surface, caractérisée par un durcissement relativement important ainsi qu'un champ de contraintes résiduelles de compression, ce qui entraîne une meilleure résistance à la fatigue. Cependant, l'effet de la vitesse d'impact de la bille et de la couverture de surface sur la modification des propriétés de surface induit par le grenaillage ne sont pas bien compris.Dans cette étude, la dureté et les contraintes résiduelles ont été étudiées en utilisant des expériences de nanoindentation pour les situations suivantes: trois vitesses de billes différentes correspondant à 35 m/s, 54 m/s et 66 m/s, ainsi que deux couvertures de surface correspondant à un seul impact et à une couverture complète (100%). Pour la situation (i) de l'étude d'un unique impact, une nouvelle procédure de polissage a été développée permettant de localiser un impact isolé. Cette procédure permet de préparer la surface de telle sorte que la nanoindentation peut être effectuée sur la section transversale de l'impact et permet de vérifier que l'impact a été produit par une bille frappant la surface avec une incidence normale. Il a été observé que la dureté et les contraintes résiduelles de compression augmentent avec une augmentation de la vitesse de la bille. Les résultats expérimentaux de contraintes résiduelles ont été comparés à ceux d'une simulation numérique en utilisant les mêmes paramètres expérimentaux de grenaillages. Il a été observé que les résultats expérimentaux montrent un comportement similaire et sont du même ordre de grandeur que ceux obtenus par simulation numérique. La principale différence est que les résultats expérimentaux ont montré une contrainte résiduelle de compression maximale étant indépendante de la vitesse de la bille.Pour la situation (ii) d'une couverture complète et à l'aide du procédé de microscopie électronique à balayage, nous avons observé un raffinement des grains adjacents à la surface grenaillée. En outre, nous avons observé que la dureté et les contraintes résiduelles de compression augmentaient avec une augmentation de la vitesse de la bille. De même que pour l'impact isolé, la localisation des contraintes résiduelles de compression maximale était indépendante de la vitesse de la bille.
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Lopez-Garrity, Omar A. "Corrosion Inhibition Mechanisms of Aluminum Alloy 2024-T3 by Selected non-Chromate Inhibitors." The Ohio State University, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=osu1372077968.

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Books on the topic "Aluminum 2024"

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

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Kolkman, H. J. Microstructural and fractographic analysis of fatigue crack propagation in 2024-T351 and 2324-T39. Amsterdam: National Aerospace Laboratory, 1985.

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Harper, Christopher Paul. Effect of alumina particle additions on the aging kinetics of 2014-aluminum matrix composites. Monterey, Calif: Naval Postgraduate School, 1991.

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E, Bennett Lawrence. Aluminum structures design manual: 2004 Florida building code : with 2006 supplements. 2nd ed. [South Daytona, FL]: L.E. Bennett (P.O. Box 214368, South Daytona 32121), 2007.

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K, Kokula Krishna Hari, ed. Investigations of Analysis and Fabrication of butt joint using friction stir welding of A319 Aluminum Alloy: ICIEMS 2014. India: Association of Scientists, Developers and Faculties, 2014.

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K, Kokula Krishna Hari, ed. Comparative Study of Gray cast Iron and Aluminum Material of Connecting Rod for Four Stroke Single Cylinder Engine: ICIEMS 2014. India: Association of Scientists, Developers and Faculties, 2014.

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K, Kokula Krshina Hari, ed. Effects of Combined Addition of Aluminum Oxide, Fly Ash, Carbon and Yttrium on Density and Hardness of ZA27 Zinc Alloy: ICIEMS 2014. India: Association of Scientists, Developers and Faculties, 2014.

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International Symposium on Gamma Titanium Aluminides (3rd 2003 San Diego, Calif.). Gamma titanium aluminides 2003: Proceedings of symposium sponsored by the Materials & Processing Committee of ASM International Materials Science Critical Technology Sector and the High Temperature Alloys Committee and the Titanium Committee of the Structural Materials Division (SMD) of TMS (The Minetals, Metals & Materials Society), held during the TMS 2004 Annual Meeting in San Diego, California, USA March 2-6, 2003. Warrendale, Penn: TMS (Minerals, Metals & Materials Society), 2003.

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N, Sharpe William, and Langley Research Center, eds. Short fatigue crack behavior in notched 2024-T3 aluminum specimens. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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Woodson, Steven Wayne. An investigation of unipolar arcing at atmospheric pressure in Aluminum 2024 and aluminum coated glass slides. 1987.

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Book chapters on the topic "Aluminum 2024"

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Vetter, Christopher, Katherine Gohmann, Alice C. Harper, and Victoria Johnston Gelling. "Polypyrrole/Aluminum Flake Hybrids as Corrosion Inhibitors for Aluminum 2024-T3." In ACS Symposium Series, 151–63. Washington, DC: American Chemical Society, 2010. http://dx.doi.org/10.1021/bk-2010-1050.ch011.

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Okoro, E., and M. N. Cavalli. "Simulated Corrosion-Fatigue via Ocean Waves on 2024-Aluminum." In Experimental and Applied Mechanics, Volume 6, 583–89. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9792-0_86.

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McEvily, A. J., Masahiro Endo, S. Cho, J. Kasivitamnuay, and Hisao Matsunaga. "Fatigue Striations and Fissures in 2024-T3 Aluminum Alloy." In Materials Science Forum, 397–400. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-469-3.397.

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Eto, Takehiko, and Manabu Nakai. "New Process-Microstructure Method for Affordable 2024 Series Aerospace Aluminum Alloys." In THERMEC 2006, 3643–48. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-428-6.3643.

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Evans, William Todd, George E. Cook, and Alvin M. Strauss. "Joining Aerospace Aluminum 2024-T4 to Titanium by Friction Stir Extrusion." In The Minerals, Metals & Materials Series, 79–89. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-52383-5_9.

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Harada, Yohei, Yutaro Sada, and Shinji Kumai. "Joining of 2024 Aluminum Alloy Stud to AZ80 Magnesium Alloy Extruded Plate by Advanced High-Speed Solid-State Method." In ICAA13: 13th International Conference on Aluminum Alloys, 771–76. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118495292.ch113.

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Milcic, Miodrag, Tomaz Vuherer, Igor Radisavljevic, and Dragan Milcic. "Experimental Investigation of Mechanical Properties on Friction Stir Welded Aluminum 2024 Alloy." In Experimental and Numerical Investigations in Materials Science and Engineering, 44–58. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-99620-2_4.

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Yost, William T., and John H. Cantrell. "The Effects of Artificial Aging of Aluminum 2024 on its Nonlinearity Parameter." In Review of Progress in Quantitative Nondestructive Evaluation, 2067–73. Boston, MA: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-2848-7_265.

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Cantrell, John H., and William T. Yost. "Nonlinear Acoustic Assessment of Precipitation-Induced Coherency Strains in Aluminum Alloy 2024." In Review of Progress in Quantitative Nondestructive Evaluation, 1361–65. Boston, MA: Springer US, 1996. http://dx.doi.org/10.1007/978-1-4613-0383-1_178.

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Mohammadi, Maysam, Ali Yazdani, Farzad Mohammadi, and Akram Alfantazi. "Corrosion Behavior of 2024 Aluminum Alloy Anodized in Sulfuric Acid Containing Inorganic Inhibitor." In Light Metals 2013, 509–13. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118663189.ch87.

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Conference papers on the topic "Aluminum 2024"

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Gilat, A., J. D. Seidt, Mark Elert, Michael D. Furnish, William W. Anderson, William G. Proud, and William T. Butler. "DYNAMIC PUNCH TESTING OF 2024-T351 ALUMINUM." In SHOCK COMPRESSION OF CONDENSED MATTER 2009: Proceedings of the American Physical Society Topical Group on Shock Compression of Condensed Matter. AIP, 2009. http://dx.doi.org/10.1063/1.3295239.

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Gilat, A., J. D. Seidt, and J. M. Pereira. "Characterization of 2024-T351 Aluminum for Dynamic Loading Applications." In 11th Biennial ASCE Aerospace Division International Conference on Engineering, Science, Construction, and Operations in Challenging Environments. Reston, VA: American Society of Civil Engineers, 2008. http://dx.doi.org/10.1061/40988(323)75.

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Wang, Hao, Yihui Huang, Zhenying Du, Wenwu Zhang, and Mengxue Bi. "Effect of Laser Shock Peening on Electrochemical Corrosion Resistance of 2024 Aluminum Alloy." In ASME 2016 11th International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/msec2016-8549.

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Laser shock peening is an innovation technique due to its significant improvement on the corrosion resistance of metallic materials. The study describes the effect of laser shock peening with multiple LSP impacts on the corrosion resistance of 2024 aluminum alloy in NaCl water solution with a mass fraction of 3.5% by using electrochemical technique. The experimental results reveal that LSP significantly reduces the corrosion rate of 2024 aluminum alloy, and as the number of impacts increases the corrosion rate decreases. The study demonstrates that LSP is an effective method to improve the electrochemical corrosion resistance of 2024 aluminum alloy.
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Shaffer, Derek, Sean Sehman, Ihab Ragai, John T. Roth, and Bin Wang. "Effect of Electrical Current on Cold Work in Aluminum 2024." In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-71090.

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Many manufacturers are looking towards electrical treatments as methods for reducing residual stresses in formed metals. Although many people have investigated the effects electricity has on residual stresses and plasticity, there has not been research investigating the effects it has as a post-treatment on strain hardening. Therefore, the goal of this research is to show the permanent changes in tensile properties that electrical treatments have on strain hardened metals, specifically Aluminum 2024. For this initial investigation, only one pulse duration and current density was used to categorize any changes in the metals due to applying electric current. This testing shows the difference between post-deformation heat treatments and post-deformation electrical treatments. Tensile properties of Aluminum 2024 were used to gauge the changes caused by the treatments. The heat treatment had the expected effect of lower the strength of the material and regrowing the grains while the electrical treatment did not seem to drastically change the structure of the grains, but still lowered the strength of the material. Microstructure investigations also showed that the material does in fact show slight changes in material properties, but no drastic changes in microstructure. These images also show that the regrowth from the heat treatment is clearly the reason for the decrease in strength.
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MANOEL CLEBER DE SAMPAIO ALVES, MARCOS VALÉRIO RIBEIRO, Marcel Yuzo Kondo, José Vitor Candido de Souza, Cleverson Pinheiro, and NATHALIA MAYUMI BERNARDES MIYAHARA. "Comparative analysis of performance tools in the aluminum 2024 turning." In 23rd ABCM International Congress of Mechanical Engineering. Rio de Janeiro, Brazil: ABCM Brazilian Society of Mechanical Sciences and Engineering, 2015. http://dx.doi.org/10.20906/cps/cob-2015-0132.

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Li, Xiaoqiang, Honghan Yu, Guiqiang Guo, and Dongsheng Li. "Single-point incremental forming of 2024-T3 aluminum alloy sheets." In NUMISHEET 2014: The 9th International Conference and Workshop on Numerical Simulation of 3D Sheet Metal Forming Processes: Part A Benchmark Problems and Results and Part B General Papers. AIP, 2013. http://dx.doi.org/10.1063/1.4850103.

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Parkhill, Robert L., and Edward T. Knobbe. "Surface texturing of aluminum alloy 2024 via excimer laser irradiation." In Photonics West '97, edited by Harry Shields and Peter E. Dyer. SPIE, 1997. http://dx.doi.org/10.1117/12.270085.

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Zhao, Xudong, Rongshi Xiao, and Kai Chen. "Study on welding of 2024 aluminum alloy sheet with disc laser." In ICALEO® 2009: 28th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2009. http://dx.doi.org/10.2351/1.5061550.

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Dou, Kai, Robert L. Parkhill, and Edward T. Knobbe. "Femtosecond pulse laser ablation and surface modification of aluminum alloy 2024." In Symposium on High-Power Lasers and Applications, edited by Santanu Basu, Steven J. Davis, and Ernest A. Dorko. SPIE, 2000. http://dx.doi.org/10.1117/12.384297.

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Hu, Cai, Yu Wang, Yun-Lai Deng, and Jian-Guo Tang. "Effects of Snake Rolling on Mechanical Properties of 2024 Aluminum Alloys." In 2016 International Conference on Mechanics and Materials Science (MMS2016). WORLD SCIENTIFIC, 2017. http://dx.doi.org/10.1142/9789813228177_0075.

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Reports on the topic "Aluminum 2024"

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Wang, Le-Min, and Chih-Jrn Tsai. Creep Resistance of 2024 Aluminum Alloy. Warrendale, PA: SAE International, October 2013. http://dx.doi.org/10.4271/2013-32-9110.

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Koch, Gerhardus H., Elise L. Hagerdorn, and Alan P. Berens. Effect of Preexisting Corrosion on Fatigue Cracking of Aluminum Alloys 2024-T3 and 7075-T6. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada430616.

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Yu, Lingyu, and Kumar V. Jata. Review and Study of Physics Driven Pitting Corrosion Modeling in 2024-T3 Aluminum Alloys (Postprint). Fort Belvoir, VA: Defense Technical Information Center, May 2015. http://dx.doi.org/10.21236/ada624864.

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Kay, G. Failure Modeling of Titanium-6Al-4V and 2024-T3 Aluminum with the Johnson-Cook Material Model. Office of Scientific and Technical Information (OSTI), September 2002. http://dx.doi.org/10.2172/15006359.

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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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Ward, Lisa, Marvin Trimm, Christopher Verst, and Sean Boland. Visual Examination of Aluminum Containers for Extended Wet Storage of Non-Aluminum-Clad Spent Nuclear Fuel (FY 2021). Office of Scientific and Technical Information (OSTI), June 2021. http://dx.doi.org/10.2172/1804668.

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