Abstract
In this chapter a brief overview of the history of Fibre Metal Laminates Arall and Glare is given as background information for the other, technical chapters of this book. This is a summary of a more complete description that can be found in [1].
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References
A. Vlot, Glare — History of the Development of a New Aircraft Material, Dordrecht: Kluwer, 2001.
R. Marissen, Fatigue crack growth in Arall a hybrid aluminium-aramid composite material, dissertation Delft University of Technology, 1988.
G. Roebroeks, Towards Glare — The development of a fatigue insensitive and damage tolerant aircraft material, dissertation Delft University of Technology, 1991.
A. Vlot, Low-velocity impact loading on fibre reinforced aluminium laminates (ARALL) and other aircraft sheet materials, dissertation Delft University of Technology, 1991.
D. Chen, Bulging of fatigue cracks in a pressurized aircraft fuselage, dissertation Delft University of Technology, 1991.
R.S. Fredell, Damage Tolerant Repair techniques for Pressrized Aircraft Fuselages, dissertation Delft University of Technology, 1994.
R.P.G. Müller, An Experimental and Analytical Investigation on the Fatigue Behaviour of Fuselage Riveted Lap Joints, dissertation Delft University of Technology, 1996.
Soerjanto Tjahjono, Consequences and Challenges of Glare for Structural Repair and Newly Designed Fuselage Structure, dissertation Delft University of Technology, 1998.
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© 2001 Springer Science+Business Media Dordrecht
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Vlot, A. (2001). Historical overview. In: Vlot, A., Gunnink, J.W. (eds) Fibre Metal Laminates. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0995-9_1
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DOI: https://doi.org/10.1007/978-94-010-0995-9_1
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-0391-2
Online ISBN: 978-94-010-0995-9
eBook Packages: Springer Book Archive