Temperature Effects on Material Behavior of Aerospace Aluminum Alloys for Subsonic and Supersonic Aircraft
Publication: Journal of Aerospace Engineering
Volume 23, Issue 2
Abstract
This review-cum-research paper reports the effects of temperature and time exposure on the material behavior of the aerospace aluminum alloys currently in use in subsonic and supersonic aircraft. The research reported in this paper involves experimental study of the microstructural characterization and temperature effects on the hardness behavior of the age-hardenable 2024-T3 aluminum alloy; the latter was acquired by one of the authors from Royal Malaysian Air Force (RMAF) aerospace industry. The ALCLAD 2024-T3 alloy is being used in C-130 Hercules aircraft by the RMAF. Recent research on various aluminum alloys being used and being considered for application in Concorde is also reviewed.
Get full access to this article
View all available purchase options and get full access to this article.
Acknowledgments
The writers are grateful to the RMAF Central Aerospace Engineering Services Establishment Division for providing the research material.
References
Anderson, R. J. (1925). The metallurgy of aluminum alloys, Henry Carey Baird & Co. Inc., New York.
Budinski, K. G., and Budinski, M. K. (2005). Engineering materials properties and selection, 8th Ed., Prentice-Hall, Upper Saddle River, N.J.
Carpenter, H. C. H., and Smith, C. C. (1923). “Tests on work-hardened aluminum sheet.” J. Inst. Met., 29, 29–66.
Carpenter, H. C. H., and Taverner, L. (1917). “The effects of heat at various temperatures on the rate of softening of cold-rolled aluminum sheet.” J. Inst. Met., 18, 115–169.
Chlistovsky, R. M., Heffernan, P. J., and DuQuesna, D. L. (2007). “Corrosion-fatigue behaviour of 7075-T651 aluminum alloy subjected to periodic overloads.” Int. J. Fatigue, 29(9–11), 1941–1949.
DeGarmo, P., Black, J. T., and Kohser. (2003). Materials and processes in manufacturing, Wiley, New York.
Dünnwald, J., and El-Magd, E. (1996). “Description of the creep behaviour of the precipitation-hardened material Al-Cu-Mg alloy 2024 using finite element computations based on microstructure mechanical models.” Comput. Mater. Sci., 7(1–2), 200–207.
Grad, C. (1919). “Traitements thernique d’ alliages d’aluminum.” Compt. Rend., 169, 571–574.
Harpur, N. F. (1968). “Concorde structural development.” J. Aircr., 5(2), 176–183.
Karabin, L. (1996). “NASA-UVA light aerospace alloy and structure technology program-supplement: Aluminum based materials for high speed aircraft.” Final Rep. Rep. No. UVA/528266/MSE96/120, Univ. of Virginia.
Kazanjian, S. M., Wang, N., and Stake, E. A., Jr. (1997). “Creep behavior and microstructural stability of Al-Cu-Mg-Ag and Al-Cu-Li-Mg-Ag alloys.” Mater. Sci. Eng., A, 234–236, 571–574.
Kosel, T., Grabec, I., and Kosel, F. (2005). “Intelligent location of two simultaneously active acoustic emission sources.” Aerosp. Sci. Technol., 9(1), 45–53.
Lee, H. T., and Shaue, G. H. (1999). “The thermomechanical behavior of aluminum alloy under uniaxial tensile loading.” Mater. Sci. Eng., A, 268(1–2), 154–164.
Majimel, J., Casanove, M. J., and Molénat, G. (2004). “A 2xxx aluminum alloy crept at medium temperature: Role of thermal activation on dislocation mechanisms.” Mater. Sci. Eng. A, 380(1–2), 110–116.
National Materials Advisory Board (NMAB). (1996). Accelerated aging of materials and structures: The effects of long-term elevated-temperature exposure, National Research Council, NMAB-479, National Academy, Washington, D.C.
Pantelakis, Sp., Kyrsanidi, An., El-Magd, E., Dünnwald, J., Barbaux, Y., and Pons, G. (1999). “Creep resistance of aluminum alloys for the next generation supersonic civil transport aircraft.” Theor. Appl. Fract. Mech., 31(1), 31–39.
Robinson, J. (2000). Next generation supersonic transport aircraft, thesis, Dept. of Materials Science and Technology, Univ. of Limerick ⟨http://www.ul.ie/~mst/research/aerospace.htm⟩.
Royal Malaysian Air Force (RMAF). (2007). CN235-220M training manual on aircraft design, pp. 1–12.
Strake, E. A., Jr. (1993). “NASA-UVA light aerospace alloy and structure technology program-supplement: Aluminum based materials for high speed aircraft.” Rep. No. 4517, NASA Conference.
Xue, Y., McDowell, D. L., Horstemeyer, M. F., Dale, M. H., and Jordon, J. B. (2007). “Microstructure-based multistage fatigue modeling of aluminum alloy 7075-T651.” Eng. Fract. Mech., 74(17), 2810–2823.
Yu, K., Li, W., Li, S., and Zhao, J. (2004). “Mechanical properties and microstructure of aluminum alloy 2618 with phases.” Mater. Sci. Eng., A, 368(1–2), 88–93.
Information & Authors
Information
Published In
Copyright
© 2010 ASCE.
History
Received: Aug 3, 2008
Accepted: May 6, 2009
Published online: May 8, 2009
Published in print: Apr 2010
Authors
Metrics & Citations
Metrics
Citations
Download citation
If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.