Designing for damage tolerance in aerospace: A hybrid material technology

Author:

Alderliesten R.C.

Publisher

Elsevier BV

Reference42 articles.

1. Pora J, Hinrichsen J. Material and technology developments for the Airbus A380. In: Proceedings of the 22nd international SAMPE Europe conference of the society for the advancement of materials and process engineering, Paris; 2001.

2. Roebroeks GHJJ. Towards GLARE – the development of a fatigue insensitive and damage tolerant aircraft material, PhD Dissertation, Delft University of Technology, Delft; 1991.

3. Fibre metal laminates – an introduction,2001

4. Marissen R. Fatigue crack growth in ARALL, a hybrid aluminium-aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate, PhD Dissertation, Delft University of Technology. ; 1998 [accessed 26.06.14].

5. Ultra high modulus carbon fibres in Arall Laminates, Memorandum M-641;Vermeeren,1990

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