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.
Oral presentation.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
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)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2011 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
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
Download citation
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
eBook Packages: EngineeringEngineering (R0)