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Journal articles on the topic '2024-T3'

Author: Grafiati

Published: 4 June 2021

Last updated: 13 February 2022

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1

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 tests, this alloy exhibited yield strength of 413 MPa, tensile strength of 527 MPa, and elongation of 15.4%. In other words, it showed higher strength than the existing alloy 2024 but was similar to the existing alloy 2024 in terms of elongation. In fatigue tests, alloy Eco-2024-T3 recorded fatigue limit of 330 MPa or around 80% of its yield strength; this is a much more excellent property compared to the existing alloy 2024-T3, which has fatigue limit of 250 MPa. Based on the aforementioned results, the correlation between the excellent mechanical properties of alloy Eco-2024-T3 and its microstructure was examined.

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2

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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3

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 former has more intensive heat generation from the plastic deformation, due to its higher strength. Friction heat generation is only slightly different for the two alloys. Therefore, temperatures in the working plate are higher in the alloy 2024 T3 for the same parameters of the plunge stage. Equivalent plastic strain is higher for 2024 T351 alloy, and the highest values are determined under the tool shoulder and around the tool pin. For the alloy 2024 T3, equivalent plastic strain is the highest in the influence zone of the tool pin.

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4

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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5

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 (December 30, 2004): 431–35. http://dx.doi.org/10.3989/revmetalm.2004.v40.i6.302.

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6

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 (April 13, 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 dan kekerasannya. Hasil penelitian menunjukkan bahwa kekasaran permukaan dan kekerasan material meningkat dengan meningkatnya intensitas peening. Namun, ketebalan Al 2524-T3, yang lebih tipis dari Al 2024-T3 menyebabkan tidak signifikannya proses peening shot yang diberikan pada material.. Kata kunci: Shot Peening, Chemical Milling, Kekerasan, Kekasaran Permukaan AbstractThis study aims to investigate the influence of shot peening on hardness and surface roughness of chemical mlling product Al 2524-T3 and Al 2024-T3 which have been stretched. These alloys were stretched beyond yield stress, namely 1%, 3% and 5% of each, and then performed chemical milling process of one side. The etching used in chemical milling process were NaOH+Na2S+H2O solutions with certain concentration. The surface was performed shot peening process with varying intensity of 0.03 A, 0.05 A and 0.07 A respectively. The material were then tested its surface roughness and hardness. The results show that surface roughness and hardness of material increases with the increase of peening intensity. However, the thickness of Al 2524–T3, which is thinner than Al 2024-T3 causing insignificance of the shot peening process given to the materials. Keywords: Shot Peening, Chemical Milling, Hardness, Surface Roughness

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7

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 softening by coarsening and dissolution of GPB zones / co-clusters or S-precipitates. Finally, the natural ageing was taken into account following the Robson model. The complete model has been calibrated with isothermal data found in the literature and still has to be optimised. Nevertheless, preliminary results show the coherence of the model when performed on isothermal data. The model has been also applied to predict FSW hardness profiles that are compared to those found in the literature.

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8

Cook, R. L., and S. R. Taylor. "Pigment-Derived Inhibitors for Aluminum Alloy 2024-T3." CORROSION 56, no. 3 (March 2000): 321–33. http://dx.doi.org/10.5006/1.3287661.

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9

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 (November 2008): 230–35. http://dx.doi.org/10.2351/1.2995769.

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10

Riveiro, A., F. Quintero, J. del Val, M. Boutinguiza, D. Wallerstein, R. Comesaña, F. Lusquiños, and J. Pou. "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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11

CHO, Shunsuke, Arthur J. MCEVILY, and Hisao MATSUNAGA. "213 Fatigue striations in 2024-T3 aluminum alloy." Proceedings of Conference of Kyushu Branch 2007 (2007): 73–74. http://dx.doi.org/10.1299/jsmekyushu.2007.73.

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12

Huda, Zainul, Nur Iskandar Taib, and Tuan Zaharinie. "Characterization of 2024-T3: An aerospace aluminum alloy." Materials Chemistry and Physics 113, no. 2-3 (February 2009): 515–17. http://dx.doi.org/10.1016/j.matchemphys.2008.09.050.

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13

Pires, I., L. Quintino, R. M. Miranda, and R. M. Miranda. "PERFORMANCE OF 2024-T3 ALUMINIUM ADHESIVE BONDED JOINTS." Materials and Manufacturing Processes 20, no. 2 (March 16, 2005): 175–85. http://dx.doi.org/10.1081/amp-200041848.

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14

Butan, Daniela, and John Monaghan. "Thermomechanical modelling friction stir welding aluminium 2024-T3." International Journal of Computational Materials Science and Surface Engineering 2, no. 1/2 (2009): 63. http://dx.doi.org/10.1504/ijcmsse.2009.024924.

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15

Vukmirovic, M. B., N. Dimitrov, and K. Sieradzki. "Dealloying and Corrosion of Al Alloy 2024-T3." Journal of The Electrochemical Society 149, no. 9 (2002): B428. http://dx.doi.org/10.1149/1.1498258.

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16

PARTL, O., and J. SCHIJVE. "Multiple-site damate in 2024-T3 alloy sheet." International Journal of Fatigue 15, no. 4 (July 1993): 293–99. http://dx.doi.org/10.1016/0142-1123(93)90378-4.

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17

Tür, Yahya K., and Öktem Vardar. "Periodic tensile overloads in 2024-T3 Al-alloy." Engineering Fracture Mechanics 53, no. 1 (January 1996): 69–77. http://dx.doi.org/10.1016/0013-7944(95)00116-d.

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18

Xie, Zong Hong, Tian Jiao Zhao, and Rui Wu. "Experimental Study on Fatigue Crack Propagation of Glare3-3/2 with Mechanics Properties." Advanced Materials Research 600 (November 2012): 273–78. http://dx.doi.org/10.4028/www.scientific.net/amr.600.273.

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This study is to investigate the fatigue crack growth behavior of Glare3-3/2 under various stress levels. The Glare3-3/2 specimen consists of three 2024-T3 aluminum alloy sheets and two layers of glass/epoxy composite lamina. Tensile-tensile cyclic fatigue tests were conducted on centrally notched specimen at four stress levels with various maximum values. A digital camera system was used to take photos of the propagating cracks on both sides of the specimen. Image processing software was adopted to accurately measure the length of the cracks on each photo. The test results show that 1) Compared to 2024-T3 aluminum alloy, the fatigue properties of Glare3-3/2 are much better: under the same loading condition with maximum stress level of 120MPa, the crack growth rate of Glare3-3/2 is roughly 5% of the corresponding value of 2024-T3 aluminum alloy, while the fatigue life is 4 times higher than that of 2024-T3 aluminum alloy. 2) The maximum stress level shows strong influence on fatigue crack propagation behavior of Glare3-3/2. The value of steady state crack growth rate increases linearly, while the number of load cycles decreases exponentially, with respect to the maximum stress values used in the fatigue tests.

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19

Leal, Rui M., and Altino Loureiro. "Microstructure and Mechanical Properties of Friction Stir Welds in Aluminium Alloys 2024-T3, 5083-O and 6063-T6." Materials Science Forum 514-516 (May 2006): 697–701. http://dx.doi.org/10.4028/www.scientific.net/msf.514-516.697.

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The aim of this research is to study the effect of the welding process on the microstructure and mechanical properties of friction stir welded joints in aluminium alloys 2024- T3, 5083-O and 6063-T6. A small loss of hardness and strength was obtained in welds in alloys 2024-T3 and 5083-O as opposed to welds in alloy 6063-T6, where a substantial softening and a drop of strength were observed. In alloy 6063-T6 a strength efficiency of only 45 to 47% was obtained.

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20

McEvily, A. J., Masahiro Endo, S. Cho, J. Kasivitamnuay, and Hisao Matsunaga. "Fatigue Striations and Fissures in 2024-T3 Aluminum Alloy." Materials Science Forum 567-568 (December 2007): 397–400. http://dx.doi.org/10.4028/www.scientific.net/msf.567-568.397.

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A study has been made of the striations and fissures developed in the aluminum alloy 2024-T3 during fatigue crack growth. Fissures were found to form on inclined facets. They were uniformly spaced as the result of a shielding process. Striation spacings were in accord with da/dN values at the higher levels of K investigated, but at low K levels striation spacings were larger than the corresponding da/dN values. The percentage of the fracture surface containing striations varied with the K level, ranging from less than 1 % at low K levels to 80 % at higher K levels. The reason for the discrepancy between the spacing of striations and the corresponding da/dN values is discussed.

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21

Pujono, Pujono. "PERPATAHAN FATIK MATERIAL ALUMINIUM 2024-T3 DENGAN PENGELASAN FSW." Infotekmesin 9, no. 01 (July 22, 2019): 30–35. http://dx.doi.org/10.35970/infotekmesin.v9i01.5.

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Resilient, machine processed, shapped aluminium using pulling power for pure aluminium with 4-5kgf/mm2. Aluminium fusion with series 2024-T3 is a metal fusion whose low weldability so it is very difficult to be conducted the welding process because it tends to occur hot cracking or being porous, and precipitation hardening when conducting welding process due to segregation of copper (Cu) fusion subtance. One of welding method to obtain the good aluminium welding result is by using FSW (friction stir welding). The purpose of this research is to find out the shape and type of fracture on aluminium fusion with FSW welding by dealing TTT. The fracture is created from fatik substance test. The reserach method was conducted by welding of plate aluminium fusion 2024-T3 using FSW technique by dealing transient thermal tensioning (TTT). Transient thermal was conducted by resigning heater line with weld tool/pin. The speed of determined FSW welding was 11 mm/minutes and 1200 rpm. The conducted test was fatigue test and factografi test with SEM. The result of the reserach shows that the number of fatik test cycle is 765.250 with sigmoidal curve visually. Then, the result of fractography using SEM shows that the occured fracture is brittle.

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22

Chen, G. S., M. Gao, and R. P. Wei. "Microconstituent-Induced Pitting Corrosion in Aluminum Alloy 2024-T3." CORROSION 52, no. 1 (January 1996): 8–15. http://dx.doi.org/10.5006/1.3292099.

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23

Kachurina, Olga, Tammy L. Metroke, and Kai Dou. "Laser-induced electrochemical characteristics of aluminum alloy 2024-T3." Journal of Laser Applications 16, no. 1 (February 2004): 46–51. http://dx.doi.org/10.2351/1.1642630.

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24

McMurray, Robert, Alan G. Leacock, and Desmond Brown. "Double Curvature Springback in Stretch Formed 2024-T3 Aluminium." Key Engineering Materials 344 (July 2007): 391–98. http://dx.doi.org/10.4028/www.scientific.net/kem.344.391.

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A test rig was developed to investigate springback in stretch draw forming processes, which are considered to be nominally uniaxial. An interchangeable tool allows the examination of both single and double curvature surfaces. Two double curvature tools with the following radii were used in the experiments, (A) 200mm by 450mm and (B) 450mm by 200mm. The first radius in each case corresponds to the direction of stretch. Obviously the smaller radius results in a larger moment, which creates a negative springback in the orthogonal direction. This effect is more pronounced in tool (A) due to the higher tensile strain levels in the direction of stretch directly affecting the strains in the orthogonal direction. By considering the resultant moment in each axis of the sheet independently, an analytical method was devised to give an approximation of the springback profile. Overall the analytical data correlates well with both experimental and Finite Element (FE) results.

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25

Cenac, François, Redouane Zitoune, Francis Collombet, and Michel Deleris. "Abrasive water-jet milling of aeronautic aluminum 2024-T3." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 229, no. 1 (August 6, 2013): 29–37. http://dx.doi.org/10.1177/1464420713499288.

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26

Milan, Růžička, Doubrava Karel, Vargas Miguel, and Kramberger Janez. "Fatigue Behaviour of Laser Machined Aluminium Alloy 2024-T3." Acta Mechanica Slovaca 15, no. 2 (October 31, 2011): 34–40. http://dx.doi.org/10.21496/ams.2011.016.

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27

Vallellano, C., C. Guzman, and J. Garcia Lomas. "Failure Prediction in Stretched Sheets of Aluminium 2024-T3." Materials Science Forum 526 (October 2006): 91–96. http://dx.doi.org/10.4028/www.scientific.net/msf.526.91.

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The present work analyses experimentally and numerically the failure limit of a 2024-T3 aluminium alloy sheet subjected to stretching. The capability of a number of ductile fracture criteria to predict sheet failure is examined and compared with experimental results. The influence of the hydrostatic pressure in the Freudenthal’s, the Cockcroft and Latham’s and the Bressan and Williams’ criterion is analyzed. The effect of the normal stress on the fracture plane in the Bressan and Williams’ criterion is also discussed.

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28

RODOPOULOS, C. A., E. R. DE LOS RIOS, A. LEVERS, and J. R. YATES. "A fatigue damage map for 2024-T3 aluminium alloy." Fatigue Fracture of Engineering Materials and Structures 26, no. 7 (July 2003): 569–75. http://dx.doi.org/10.1046/j.1460-2695.2003.00526.x.

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29

Yisheng, W., and J. Schijve. "FATIGUE CRACK CLOSURE MEASUREMENTS ON 2024-T3 SHEET SPECIMENS." Fatigue & Fracture of Engineering Materials & Structures 18, no. 9 (April 2, 2007): 917–21. http://dx.doi.org/10.1111/j.1460-2695.1995.tb00916.x.

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30

Hughes, A. E., G. Theodossiou, S. Elliott, T. G. Harvey, P. R. Miller, J. D. Gorman, and P. J. K. Paterson. "Study of deoxidation of 2024-T3 with various acids." Materials Science and Technology 17, no. 12 (December 2001): 1642–52. http://dx.doi.org/10.1179/026708301101509728.

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31

Lin, Y. C., Yu-Chi Xia, Ming-Song Chen, Yu-Qiang Jiang, and Lei-Ting Li. "Modeling the creep behavior of 2024-T3 Al alloy." Computational Materials Science 67 (February 2013): 243–48. http://dx.doi.org/10.1016/j.commatsci.2012.09.007.

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32

Jones, Kimberli, and David W. Hoeppner. "Prior corrosion and fatigue of 2024-T3 aluminum alloy." Corrosion Science 48, no. 10 (October 2006): 3109–22. http://dx.doi.org/10.1016/j.corsci.2005.11.008.

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33

Gruenberg, K. "Predicting fatigue life of pre-corroded 2024-T3 aluminum." International Journal of Fatigue 26, no. 6 (June 2004): 629–40. http://dx.doi.org/10.1016/j.ijfatigue.2003.10.011.

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34

Drewien, C. A., R. G. Buchheit, K. R. Zavadil, and T. E. Neil. "Copper enrichment on Al 2024 surface after de-oxidizing treatment." Proceedings, annual meeting, Electron Microscopy Society of America 51 (August 1, 1993): 860–61. http://dx.doi.org/10.1017/s0424820100150137.

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Coatings of lithium-aluminum-carbonate-hydroxide are being developed for corrosion protection of aluminum alloys against atmospheric and saline environments. Coating is performed by immersion of the aluminum part into a lithium carbonate-lithium hydroxide solution of pH=11.5. Before coating, the aluminum alloy is degreased in trichloroethylene, cleaned in a sodium carbonate-sodium silicate bath, and de-oxidized in nitric acid containing ammonium biflouride. Coating of most aluminum alloys is easily accomplished, and the coatings pass the ASTM B117 salt spray test. However, aluminum alloys that contain copper, specifically 2024-T3 and 7075-T6, yield coatings that fail the salt spray test, i.e. pitting and general corrosion is observed. Photographs of coatings after 168 hr salt spray exposure are shown in Figure 1 for Al 1100 and 2024-T3 alloys. A study has been undertaken to determine the influence of copper upon the corrosion properties of the coating.The surface of 2024-T3 was analyzed after each processing step in order to determine if copper enrichment at the specimen surface was occurring.

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35

Kubit, A., R. Kluz, K. Ochałek, D. Wydrzyński, and T. Trzepieciński. "Friction stir welding of 2024-T3 aluminium alloy sheet with sheet pre-heating." Materiali in tehnologije 52, no. 3 (June 6, 2018): 283–88. http://dx.doi.org/10.17222/mit.2017.084.

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36

Jiang, Wei, Ya Zhi Li, Yi Xiu Shu, and Masanori Kikuchi. "Mechanism-Based Numerical Approach to Ductile Fracture in an 2024–T3 Aluminium Alloy." Applied Mechanics and Materials 627 (September 2014): 74–78. http://dx.doi.org/10.4028/www.scientific.net/amm.627.74.

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Ductile fracture of 2024-T3 aluminum alloy has been investigated under tensile and shear loading conditions. In order to predict rupture, a void–based meso–damage constitutive relationship which can deal with both tensile and shear problems is developed and implemented in commercial software ABAQUS. The tensile and shear fracture behaviors including the load–displacement response and crack propagation path, of 2024–T3 aluminum alloy are analyzed using the proposed approach and compared with experimental data. It is shown that the proposed approach can be used to predict the failure of ductile materials under complex loading conditions.

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37

Chen, Lei. "Numerical Simulation and Experiment of Aluminum Sheet Metal Springback in New Quenching State." Advanced Materials Research 97-101 (March 2010): 2567–70. http://dx.doi.org/10.4028/www.scientific.net/amr.97-101.2567.

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2024-T3 aluminium sheet metal rubber forming process after quenching is studied. The tensile properties of 2024-T3 after quenching are measured. It is found that the yield strength and ultimate tensile strength are reduced, whilst total elongation value is increased. Springback character of rubber forming is studied by numerical method and springback compensation of rib flanging is studied. The simulation is compared with experiment. It is found that the tool shape considering springback is got using numerical method. The parts after springback achieve the design accuracy. So the method can be used in the application of rubber net forming.

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38

Smith, Bert L., Tanya L. Z. Flores, and Ala L. Hijazi. "Link-Up Strength of 2524-T3 and 2024-T3 Aluminum Panels with Multiple Site Damage." Journal of Aircraft 42, no. 2 (March 2005): 535–41. http://dx.doi.org/10.2514/1.4211.

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39

Zamber, J. E., and B. M. Hillberry. "Probabilistic Approach to Predicting Fatigue Lives of Corroded 2024-T3." AIAA Journal 37, no. 10 (October 1999): 1311–17. http://dx.doi.org/10.2514/2.602.

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40

Smith, Bert L., Perry A. Saville, Adil Mouak, and Roy Y. Myose. "Strength of 2024-T3 Aluminum Panels with Multiple Site Damage." Journal of Aircraft 37, no. 2 (March 2000): 325–31. http://dx.doi.org/10.2514/2.2597.

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Lopez-Garrity, O., and G. S. Frankel. "Corrosion Inhibition of Aluminum Alloy 2024-T3 by Praseodymium Chloride." CORROSION 70, no. 9 (September 2014): 928–41. http://dx.doi.org/10.5006/1244.

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Salim, Basheer H. Khudair, Fadhel A. Hashim, Raid K. "Effect of Friction Stir Processing on (2024-T3) Aluminum Alloy." International Journal of Innovative Research in Science, Engineering and Technology 04, no. 03 (March 15, 2015): 1822–29. http://dx.doi.org/10.15680/ijirset.2015.0404003.

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Hughes, A. E., J. D. Gorman, T. G. Harvey, A. Galassi, and G. McAdam. "Development of Permanganate-Based Coatings on Aluminum Alloy 2024-T3." CORROSION 62, no. 9 (September 2006): 773–80. http://dx.doi.org/10.5006/1.3278302.

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Hu, Tianhui, Hongwei Shi, Tao Wei, Fuchun Liu, Shihua Fan, and En-Hou Han. "Cerium tartrate as a corrosion inhibitor for AA 2024-T3." Corrosion Science 95 (June 2015): 152–61. http://dx.doi.org/10.1016/j.corsci.2015.03.010.

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Whitten, Mary C., and Chhiu-Tsu Lin. "An in situ phosphatizing coating on 2024 T3 aluminum coupons." Progress in Organic Coatings 38, no. 3-4 (June 2000): 151–62. http://dx.doi.org/10.1016/s0300-9440(00)00101-6.

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Lin, Y. C., Yu-Chi Xia, Yu-Qiang Jiang, Hua-Min Zhou, and Lei-Ting Li. "Precipitation hardening of 2024-T3 aluminum alloy during creep aging." Materials Science and Engineering: A 565 (March 2013): 420–29. http://dx.doi.org/10.1016/j.msea.2012.12.058.

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Sutton, M. A., B. Yang, A. P. Reynolds, and R. Taylor. "Microstructural studies of friction stir welds in 2024-T3 aluminum." Materials Science and Engineering: A 323, no. 1-2 (January 2002): 160–66. http://dx.doi.org/10.1016/s0921-5093(01)01358-2.

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Carpio, F. "Fatigue behaviour of laser machined 2024 T3 aeronautic aluminium alloy." Applied Surface Science 208-209 (March 15, 2003): 194–98. http://dx.doi.org/10.1016/s0169-4332(02)01369-7.

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Ramos, Jorge A., J. Magee, and K. G. Watkins. "Microstructure and microhardness study of laser bent Al-2024-T3." Journal of Laser Applications 13, no. 1 (February 2001): 32–40. http://dx.doi.org/10.2351/1.1340339.

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Zamber, J. E., and B. M. Hillberry. "Probabilistic approach to predicting fatigue lives of corroded 2024-T3." AIAA Journal 37 (January 1999): 1311–17. http://dx.doi.org/10.2514/3.14323.

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