Abstract
This chapter tries to answer the question: “How do we improve the Glare properties by searching for the most relevant aluminium alloy?” First, a quick overview of the available improvements made in the aluminium industry is given. A brief summarisation of the influence of the aluminium alloy properties upon the residual strength of the laminate follows, and finally the new aluminium alloys most promising for Glare are presented.
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References
Ph. Lequeu, et al., Int. Journal of Aircraft Engineering and Aerospace Technology. Volume 73. 2001.
G. Jay, Comparison of the damage tolerance behavior of two aluminium alloys: 2024 and 2024 A. TU Delft, 2000.
Tj. de Vries, Residual Strength Design Tool for Glare. Internal report. TU Delft, 2000.
R. Dif, et al., Proceedings of the ICAA6 Conference. Japan: Toyoashi, July 1998.
J. Liu, et al., A New Paradigm In The Design of Aluminium Alloys for Aerospace Applications. ICCA7, 2000.
M. Hagenbeek, Feasibility of Tsai-Hill critérium for yield and ultimate strength of unnotched material. Memorandum. TU Delft, 2001.
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© 2001 Springer Science+Business Media Dordrecht
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Auffret, A., Gennai, A. (2001). New aluminium alloys for Glare. In: Vlot, A., Gunnink, J.W. (eds) Fibre Metal Laminates. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0995-9_6
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DOI: https://doi.org/10.1007/978-94-010-0995-9_6
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-0391-2
Online ISBN: 978-94-010-0995-9
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