Abstract
This paper presents and discusses some of the recent advancements that have been achieved in the development of the FML concept for thin single-aisle fuselage structures. It is shown that the inherent damage tolerant nature of this concept can be further exploited for these structural applications.
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References
de Vries, T.J.: Blunt and sharp notch behaviour of Glare laminates, PhD dissertation, Delft University of Technology (2001)
Lucas, C.: Static, fatigue and damage tolerance behaviour of the Fibre Metal Laminate GLARE based on the new aluminium lithium alloy: 1441-T11, Thesis, Delft University of Technology (2010)
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© 2011 Springer-Verlag Berlin Heidelberg
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Alderliesten, R.C., Rans, C.D., Beumler, T., Benedictus, R. (2011). Recent Advancements in Thin-Walled Hybrid Structural Technologies for Damage Tolerant Aircraft Fuselage Applications. In: Komorowski, J. (eds) ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives. Springer, Dordrecht. https://doi.org/10.1007/978-94-007-1664-3_8
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DOI: https://doi.org/10.1007/978-94-007-1664-3_8
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-007-1663-6
Online ISBN: 978-94-007-1664-3
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