An Historic Overview of the Development of Fibre Metal Laminates

Applied Composite Materials

Volumn 10, Issue 4-5, 2003, Pages 189-205

  Vermeeren, C A J R ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

3M; Akzo; Alcoa; Arall; Ballistic material; Barrel test; Burn through; Delft University; Fibre Metal Laminates; Fokker; Glare; Residual strength; Static properties; Structural Laminates Company

Indexed keywords

ADHESIVES; ALUMINUM; GLASS FIBERS;

FIBER METAL LAMINATES;

LAMINATED COMPOSITES;

EID: 0142007778     PISSN: 0929189X     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1025533701806     Document Type: Review

References (8)

1. Vlot, A., Glare - History of the Development of a New Aircraft Material, Dordrecht, Kluwer, 2001.
2. Marissen, R., Fatigue Crack Growth in Arall a Hybrid Aluminium-Aramid Composite Material, Dissertation, Delft University of Technology, 1988.
3. Roebroeks, G., Towards Glare - The Development of a Fatigue Insensitive and Damage Tolerant Aircraft Material, Dissertation, Delft University of Technology, 1991.
4. Chen, D., Bulging of Fatigue Cracks in a Pressurized Aircraft Fuselage, Dissertation, Delft University of Technology, 1991.
5. Vermeeren, C. A. J. R., 'The Residual Strength of Fibre Metal Laminates. ' PhD thesis, Delft University of Technology, 1995.
6. de Vries, T. J., 'Blunt and Sharp Notch Behaviour of Glare Laminates,' PhD thesis, Delft University of Technology, 2001.
7. Fredell, R. S., Damage Tolerant Repair Techniques for Pressrized Aircraft Fuselages, Dissertation, Delft University of Technology, 1994.
8. Tjahjono, S., Consequences and Challenges of Glare for Structural Repair and Newly Designed Fuselage Structure, Dissertation, Delft University of Technology, 1998.