Relevant bibliographies by topics / 2024-T3

Contents

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

Academic literature on the topic '2024-T3'

Author: Grafiati
Published: 4 June 2021
Last updated: 13 February 2022

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Journal articles on the topic "2024-T3"

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Kim, Seon Ho, Kyu Sik Kim, Shae K. Kim, Young Ok Yoon, Kyu Sang Cho, and Kee Ahn Lee. "Microstructure and Mechanical Properties of Eco-2024-T3 Aluminum Alloy." Advanced Materials Research 602-604 (December 2012): 623–26. http://dx.doi.org/10.4028/www.scientific.net/amr.602-604.623.

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In this study, the microstructures and mechanical properties of the recently developed Eco-2024-T3 alloy were examined. Eco-2024 is made using Eco-Mg (Mg-Al2Ca) in place of element Mg during the manufacture of alloy 2024-T3. This is an alloy that has economic advantage and excellent properties. Alloy Eco-2024 showed smaller crystal grains that were distributed more evenly compared to the existing alloy 2024-T3. It consisted of Al matrices containing minute amounts of Al2CuMg, Al2Cu, and Ca phases and showed microstructures with reduced amounts of Fe phases or oxide. As a result of tensile test
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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 (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 peneli
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Veljic, Darko, Bojan Medjo, Marko Rakin, Zoran Radosavljevic, and Nikola Bajic. "Analysis of the tool plunge in friction stir welding - comparison of aluminium alloys 2024 T3 and 2024 T351." Thermal Science 20, no. 1 (2016): 247–54. http://dx.doi.org/10.2298/tsci150313059v.

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Temperature, plastic strain and heat generation during the plunge stage of the friction stir welding (FSW) of high-strength aluminium alloys 2024 T3 and 2024 T351 are considered in this work. The plunging of the tool into the material is done at different rotating speeds. A three-dimensional finite element (FE) model for thermomechanical simulation is developed. It is based on arbitrary Lagrangian-Eulerian formulation, and Johnson-Cook material law is used for modelling of material behaviour. From comparison of the numerical results for alloys 2024 T3 and 2024 T351, it can be seen that the for
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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 (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 Amp
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Monslave, A., and R. Morales. "Caracterización de la respuesta a fractura de las aleaciones de aluminio 2024-O y 2024-T3." Revista de Metalurgia 40, no. 6 (2004): 431–35. http://dx.doi.org/10.3989/revmetalm.2004.v40.i6.302.

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Mahyoedin, Yovial, Jamasri Jamasri, Rizky Arman, Wenny Marthiana, and Suryadima Suryadima. "Pengaruh Shot Peening Terhadap Kekerasan Dan Kekasaran Produk Chemical Milling Paduan Aluminium Yang Telah Di Stretching." JURNAL KAJIAN TEKNIK MESIN 5, no. 1 (2020): 36–41. http://dx.doi.org/10.52447/jktm.v5i1.2995.

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AbstrakPenelitian ini bertujuan untuk mengetahui pengaruh shot peening terhadap kekasaran permukaan produk pembuatan kimia Al 2524-T3 dan Al 2024-T3 yang telah diregangkan. Paduan ini direntangkan melampaui tegangan luluh, yaitu masing-masing 1%, 3% dan 5%, dan kemudian dilakukan proses penggilingan kimia di satu sisi. Etching yang digunakan dalam proses penggilingan kimia adalah larutan NaOH + Na2S + H2O dengan konsentrasi tertentu. Permukaan dilakukan proses shot peening dengan intensitas yang bervariasi masing-masing 0,03 A, 0,05 A dan 0,07 A. Bahan itu kemudian diuji kekasaran permukaan da
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Galisson, Sébastien, Denis Carron, Philippe Le Masson, Georgios Stamoulis, Eric Feulvarch, and Gilles Surdon. "Hardness Prediction of AA 2024-T3 FSW Weld." Materials Science Forum 1016 (January 2021): 1857–62. http://dx.doi.org/10.4028/www.scientific.net/msf.1016.1857.

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The hardness of AA 2024 is mainly dependent of the precipitation state in the material. This one will vary through the process of friction stir welding (FSW) which generates heat and deformations. The most important effect will be the thermal excursion which greatly affects the nature and the distribution of precipitates and so the mechanical properties of the material. Three Myhr & Grong-type submodels have been used in this study in order to simulate the variation of hardness in AA 2024-T3 FSW welds. These models allowed to simulate the hardening by growth of S-precipitates and the softe
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Cook, R. L., and S. R. Taylor. "Pigment-Derived Inhibitors for Aluminum Alloy 2024-T3." CORROSION 56, no. 3 (2000): 321–33. http://dx.doi.org/10.5006/1.3287661.

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Riveiro, A., F. Quintero, F. Lusquiños, J. Pou, and M. Pérez-Amor. "Laser cutting of 2024-T3 aeronautic aluminum alloy." Journal of Laser Applications 20, no. 4 (2008): 230–35. http://dx.doi.org/10.2351/1.2995769.

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Riveiro, A., F. Quintero, J. del Val, et al. "Laser cutting of aluminum alloy Al-2024-T3." Procedia Manufacturing 13 (2017): 396–401. http://dx.doi.org/10.1016/j.promfg.2017.09.028.

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Dissertations / Theses on the topic "2024-T3"

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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
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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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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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Petersen, Amanda de Moura. "Comportamento inibidor da corrosão de antocianinas na liga de alumínio 2024-T3." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2016. http://hdl.handle.net/10183/153271.

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A eficiência de antocianinas como inibidores de corrosão da liga de alumínio 2024-T3 foi avaliada através de medidas eletroquímicas como a espectroscopia de impedância eletroquímica e polarizações anódica e catódica. Soluções de NaCl 0,025 mol.L-1 contendo diferentes concentrações (800, 1000, 2000, 3000, 5000 e 7200 ppm) de antocianinas extraídas da uva foram preparadas para analisar o efeito da presença destas substâncias quando em contato com a liga de alumínio 2024-T3. Medidas de espectroscopia de impedância eletroquímica apresentaram uma diminuição sobre a dispersão dos pontos nas regiões
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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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Tamborim, Takeuchi Silvia Margonei Mesquita. "Revestimentos anticorrosivos à base de silanos sobre a liga de alumínio 2024-T3." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2009. http://hdl.handle.net/10183/16169.

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Revestimentos de silanos foram depositados sobre a liga de alumínio 2024 - T3 a fim de avaliar a sua utilização como revestimento protetor à corrosão. O capítulo I trata sobre o estudo do comportamento corrosivo de tratamentos baseados na deposição de camadas de 3-(trimetoxisililpropilmetacrilato (TMSPM) e/ou nitrato de cério sobre a liga de alumínio 2024 T-3 (AA2024 T-3). A resistência à corrosão foi avaliada por espectroscopia de impedância eletroquímica (EIE) durante a imersão em soluções de NaCl e Na2SO4 0,1molL-¹. Microscopia de força atômica (AFM), microscopia eletrônica de varredura (ME
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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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Boag, Adam Paull, and adam boag@gmail com. "The Relationship Between Microstructure and Stable Pitting Initiation in Aerospace Aluminium Alloy 2024-T3." RMIT University. Applied Science, 2009. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20091028.114831.

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Aluminium alloys are essential to a variety of industry sectors, particularly transport, where they are used in the production of cars and aeroplanes. However, aluminium alloys are susceptible to degradation through corrosion which can compromise the integrity of components manufactured from this material. Therefore research into the means by which these alloys degrade is important. This thesis aims to understand how one of the more potentially damaging types of corrosion, known as pitting corrosion, occurs in the important aluminium alloy 2024-T3 (AA2024-T3). In order to study this pheno
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Chilukuri, Anusha. "Corrosion Inhibition by Inorganic Cationic Inhibitors on the High Strength Aluminum Alloy, 2024-T3." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1343784869.

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Elaish, Reafat. "Influences of fluorine species on the anodizing behaviour of aluminium and AA 2024-T3 alloy." Thesis, University of Manchester, 2018. https://www.research.manchester.ac.uk/portal/en/theses/influences-of-fluorine-species-on-the-anodizing-behaviour-of-aluminium-and-aa-2024t3-alloy(7849513e-31b6-4f71-a6ee-126ee5221321).html.

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The present study investigates the effect of fluorine species during anodizing of aluminium and AA2024-T3 alloy in sulphuric acid and tartaric-sulphuric acid (TSA) electrolytes. The investigation comprises four main parts; (i) Effects of fluoride on barrier film formation on aluminium. (ii) Effects of fluoride and fluorozirconic acid (FZ) on porous film growth on aluminium in sulphuric acid. (iii) Effects of FZ on porous film growth on aluminium and AA 2024-T3 alloy in sulphuric acid and TSA. (iv) Effects on anodizing of other fluoroacids (fluoroboric (FB), fluorosilicic (FS) and fluorotitanic
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Books on the topic "2024-T3"

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Center, Langley Research, ed. Multi-lab comparison of R-curve methodologies: Alloy 2024-T3. National Aeronautics and Space Administration, Langley Research Center, 1994.

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Center, Langley Research, ed. Multi-lab comparison of R-curve methodologies: Alloy 2024-T3. National Aeronautics and Space Administration, Langley Research Center, 1994.

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

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Multi-lab comparison of R-curve methodologies: Alloy 2024-T3. National Aeronautics and Space Administration, Langley Research Center, 1994.

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S, Dawicke D., and Langley Research Center, eds. An evaluation of the pressure proof test concept for thin sheet 2024-T3. National Aeronautics and Space Administration, Langley Research Center, 1990.

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An evaluation of the pressure proof test concept for thin sheet 2024-T3. National Aeronautics and Space Administration, Langley Research Center, 1990.

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C, Newman J., and Langley Research Center, eds. Prediction of stable tearing of 2024-T3 aluminum alloy using the crack-tip opening angle approach. National Aeronautics and Space Administration, Langley Research Center, 1993.

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C, Newman J., and Langley Research Center, eds. Prediction of stable tearing of 2024-T3 aluminum alloy using the crack-tip opening angle approach. National Aeronautics and Space Administration, Langley Research Center, 1993.

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Center, Langley Research, ed. Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1997.

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Center, Langley Research, ed. Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1997.

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Book chapters on the topic "2024-T3"

1

Olfa, Daghfas, Znaidi Amna, Gahbiche Amen, and Nasri Rachid. "Plastic Behavior of 2024-T3 Under Uniaxial Shear Tests." In Design and Modeling of Mechanical Systems—III. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-66697-6_102.

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McMurray, Robert, Alan Leacock, and Desmond Brown. "Double Curvature Springback in Stretch Formed 2024-T3 Aluminium." In Sheet Metal 2007. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-437-5.391.

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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. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-469-3.397.

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Vallellano, C., C. Guzman, and J. Garcia Lomas. "Failure Prediction in Stretched Sheets of Aluminium 2024-T3." In Materials Science Forum. Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-417-0.91.

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Pastor, M. L., X. Balandraud, J. L. Robert, and M. Grédiac. "Fatigue Properties of 2024-T3 Aluminium Specimens Reinforced With Composite Patches." In Experimental Analysis of Nano and Engineering Materials and Structures. Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6239-1_66.

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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. American Chemical Society, 2010. http://dx.doi.org/10.1021/bk-2010-1050.ch011.

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Sano, Tomoko, C. Fountzoulas, C. F. Yen, C. Chen, and M. Nansteel. "Failure Characterization of AA 2024 T3 Panel Subjected to Close-In Blast." In Dynamic Behavior of Materials, Volume 1. Springer New York, 2012. http://dx.doi.org/10.1007/978-1-4614-4238-7_36.

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McMurray, Robert, Alan Leacock, and Desmond Brown. "The Influence of Cladding on the Springback of 2024-T3 Aluminium Alloy." In Engineering Plasticity and Its Applications. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-433-2.853.

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Huang, Hong, Qingyun Zhao, and Fenglei Liu. "Effect of Strengthened Hole on the Fatigue Life of 2024-T3 Aluminum Alloy." In ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-21503-3_48.

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Okada, T., K. Kuwayama, S. Fujita, M. Asakawa, T. Nakamura, and S. Machida. "Properties Of Fatigue Crack Propagation In Friction Stir Welded 2024-T3 Aluminum Alloy." In ICAF 2009, Bridging the Gap between Theory and Operational Practice. Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-2746-7_48.

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Conference papers on the topic "2024-T3"

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Riveiro, A., J. Pou, F. Lusquiños, et al. "Laser cutting of 2024-T3 aeronautic aluminium alloy." In ICALEO® 2006: 25th International Congress on Laser Materials Processing and Laser Microfabrication. Laser Institute of America, 2006. http://dx.doi.org/10.2351/1.5060829.

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Nair, R. Madhavan, B. Durairajan, and B. Bahr. "High Speed Drilling of Al-2024-T3 Alloy." In General Aviation Technology Conference & Exhibition. SAE International, 2002. http://dx.doi.org/10.4271/2002-01-1516.

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Ramos, J. A., J. Magee, K. Watkins, W. M. Steen, and F. Noble. "Microstructure of laser bent aluminium alloy Alclad 2024-T3." In ICALEO® ‘98: Proceedings of the Laser Materials Processing Conference. Laser Institute of America, 1998. http://dx.doi.org/10.2351/1.5059146.

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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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Casalino, G., L. A. C. De Filippis, and A. D. Ludovico. "On CO2 laser welding of Al 2024-T3 and Al 8090-T3 aluminium alloys butt joints." In ICALEO® 2001: Proceedings of the Laser Materials Processing Conference and Laser Microfabrication Conference. Laser Institute of America, 2001. http://dx.doi.org/10.2351/1.5059769.

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Zamber, J., and B. Hillberry. "A probabilistic approach to predicting fatigue lives of corroded 2024-T3." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2054.

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Alves Correa, Pedro Henrique, Renner Egalon Pereira, and Jorge Alberto Rodriguez Duran. "Spectral fatigue analysis for Al 2024-T3 with nonzero mean stress." In 7th International Symposium on Solid Mechanics. ABCM, 2019. http://dx.doi.org/10.26678/abcm.mecsol2019.msl19-0163.

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Kuwayama, Kazuya, Motoo Asakawa, Takao Okada, Toshiya Nakamura, Shigeru Machida, and Shinya Fujita. "Fatigue Crack Propagation Property of Friction Stir Welded 2024-T3 Aluminum Alloy." In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2619.

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Siddiqui, M. H., F. Hashmi, and A. Junaid. "Determination of anisotropy in impact toughness of aluminium alloy 2024 T3 plate." In 2013 IEEE Aerospace Conference. IEEE, 2013. http://dx.doi.org/10.1109/aero.2013.6496891.

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Wahab, M. A., J. H. Park, and S. S. Pang. "Corrosion Prevention Compound on the Fatigue Life of 2024-T3 Aluminum Alloy." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-82906.

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Corrosion-Prevention-Compounds (CPC) are commonly used to prevent corrosion in the aircraft industry. The presence of corrosive environment on aircraft structures has detrimental effects on the aircraft components which reduces the fatigue life and may also accelerate the crack growth rate in the structures. This is an experimental study on 2024-T3 aluminum alloy to investigate the effect of fatigue crack growth (life from threshold crack growth to final failure) using CPC on fatigue life. The corrosion fatigue with the presence of water-vapor reduces the total fatigue life. The fatigue life w
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Reports on the topic "2024-T3"

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Leseur, D. Experimental investigations of material models for Ti-6A1-4V and 2024-T3. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/11977.

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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. Defense Technical Information Center, 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). Defense Technical Information Center, 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), 2002. http://dx.doi.org/10.2172/15006359.

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